Explore: Aeroacoustics
Discover books, insights, and more — all in one place.
Learn more about Aeroacoustics with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “aeroacoustics”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Quadrature-free implementation of discontinuous Galerkin method for hyperbolic equations
By H. L. Atkins
“Quadrature-free implementation of discontinuous Galerkin method for hyperbolic equations” Metadata:
- Title: ➤ Quadrature-free implementation of discontinuous Galerkin method for hyperbolic equations
- Author: H. L. Atkins
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration , Langley Research Center - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Quadrature-free implementation of discontinuous Galerkin method for hyperbolic equations” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Boundary value problems - Differential equations, Hyperbolic - Finite element method - Galerkin method - Galerkin methods - Hyperbolic Differential equations - Robustness (Mathematics) - Unstructured grids (Mathematics)
Edition Identifiers:
- The Open Library ID: OL17126166M - OL18121504M - OL17593389M - OL15505075M - OL19141403M
- Online Computer Library Center (OCLC) ID: 40120203
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Quadrature-free implementation of discontinuous Galerkin method for hyperbolic equations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Two-dimensional fourier transform applied to helicopter flyover noise
By Odilyn L. Santa Maria
“Two-dimensional fourier transform applied to helicopter flyover noise” Metadata:
- Title: ➤ Two-dimensional fourier transform applied to helicopter flyover noise
- Author: Odilyn L. Santa Maria
- Language: English
- Number of Pages: Median: 52
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Hampton, Va - Hampton, VA - Springfield, VA - Hanover, Md
“Two-dimensional fourier transform applied to helicopter flyover noise” Subjects and Themes:
- Subjects: ➤ Helicopters - Aeroacoustics - Fourier transformation - Aircraft noise - Aerodynamic noise - Fourier analysis - Noise - Harmonic analysis - Fourier transformations - Noise control
Edition Identifiers:
- The Open Library ID: OL19264016M - OL17591908M - OL18134997M - OL15548984M - OL17135076M
- Online Computer Library Center (OCLC) ID: 42686523
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Two-dimensional fourier transform applied to helicopter flyover noise at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3High-accuracy compact MacCormack-type schemes for computational aeroacoustics
By R. Hixon
“High-accuracy compact MacCormack-type schemes for computational aeroacoustics” Metadata:
- Title: ➤ High-accuracy compact MacCormack-type schemes for computational aeroacoustics
- Author: R. Hixon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service [distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, VA - Cleveland, Ohio
“High-accuracy compact MacCormack-type schemes for computational aeroacoustics” Subjects and Themes:
- Subjects: Screech tones - Aircraft noise - Aeroacoustics - Matrices (Mathematics)
Edition Identifiers:
- The Open Library ID: OL18134460M - OL17133282M - OL15547001M - OL17595613M
- Online Computer Library Center (OCLC) ID: 42075914
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find High-accuracy compact MacCormack-type schemes for computational aeroacoustics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Essentially non-oscillatory and weighted essentially non-oscillatory schemes for hyperbolic conservation laws
By Chi-Wang Shu
“Essentially non-oscillatory and weighted essentially non-oscillatory schemes for hyperbolic conservation laws” Metadata:
- Title: ➤ Essentially non-oscillatory and weighted essentially non-oscillatory schemes for hyperbolic conservation laws
- Author: Chi-Wang Shu
- Language: English
- Number of Pages: Median: 78
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, VA - Springfield, VA
“Essentially non-oscillatory and weighted essentially non-oscillatory schemes for hyperbolic conservation laws” Subjects and Themes:
- Subjects: ➤ Turbulence - Aeroacoustics - Nonlinearity - Essentially non-oscillatory schemes - Finite difference theory - Finite differences - Mathematical models - Hamilton-Jacobi equations - Numerical solutions - Nonlinear theories
Edition Identifiers:
- The Open Library ID: OL19288625M - OL17582187M - OL17132061M - OL15547173M
- Online Computer Library Center (OCLC) ID: 41618360
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Essentially non-oscillatory and weighted essentially non-oscillatory schemes for hyperbolic conservation laws at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Reduction of Blade-Vortex Interaction (BVI) noise through X-force control
By Fredric H. Schmitz
“Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” Metadata:
- Title: ➤ Reduction of Blade-Vortex Interaction (BVI) noise through X-force control
- Author: Fredric H. Schmitz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Reduction of Blade-Vortex Interaction (BVI) noise through X-force control” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft landing - Blade slap noise - Blade-vortex interaction - Flight control - Flight paths - Helicopters - Inlet flow - Longitudinal stability - Noise prediction (Aircraft) - Noise reduction
Edition Identifiers:
- The Open Library ID: OL18087419M - OL15424058M - OL17106597M - OL17117531M
- Online Computer Library Center (OCLC) ID: 35280105
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Reduction of Blade-Vortex Interaction (BVI) noise through X-force control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Acoustic treatment design scaling methods
By R. E. Kraft
“Acoustic treatment design scaling methods” Metadata:
- Title: ➤ Acoustic treatment design scaling methods
- Author: R. E. Kraft
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999 - 2003
- Publish Location: ➤ - Hanover, MD - [Springfield, Va - Hampton, Va
“Acoustic treatment design scaling methods” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - High frequencies - Mathematical models - Aircraft models - Scale models - Aircraft engines - Acoustic impedance - Frequency ranges - Aircraft noise - Noise prediction (Aircraft) - Impedance measurement - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL17621421M - OL17722881M - OL15554930M - OL17584196M
- Online Computer Library Center (OCLC) ID: 54914469 - 42269573
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Acoustic treatment design scaling methods at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7The method of space-time conservation element and solution element-applications to one-dimensional and two-dimensional time-marching flow problems
By Sin-Chung Chang
“The method of space-time conservation element and solution element-applications to one-dimensional and two-dimensional time-marching flow problems” Metadata:
- Title: ➤ The method of space-time conservation element and solution element-applications to one-dimensional and two-dimensional time-marching flow problems
- Author: Sin-Chung Chang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“The method of space-time conservation element and solution element-applications to one-dimensional and two-dimensional time-marching flow problems” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aeroacoustics - Space-time functions - Relativity - Two dimensional flow - One dimensional flow - Conservation laws - Euler equations of motion - Time marching
Edition Identifiers:
- The Open Library ID: OL15413483M - OL18081079M - OL17015900M
- Online Computer Library Center (OCLC) ID: 33470358
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The method of space-time conservation element and solution element-applications to one-dimensional and two-dimensional time-marching flow problems at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Computing jet screech--a complex aeroacoustic feedback system
By Ching Y. Loh
“Computing jet screech--a complex aeroacoustic feedback system” Metadata:
- Title: ➤ Computing jet screech--a complex aeroacoustic feedback system
- Author: Ching Y. Loh
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2002
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Computing jet screech--a complex aeroacoustic feedback system” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Feedback - Noise (Sound) - Numerical analysis - Screech tones - Sound waves
Edition Identifiers:
- The Open Library ID: OL21783551M - OL17621437M - OL16111174M - OL18215631M
- Online Computer Library Center (OCLC) ID: 55957123
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Computing jet screech--a complex aeroacoustic feedback system at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Acoustics, Aeroacoustics and Vibrations
By Fabien Anselmet and Pierre-Olivier Mattei
“Acoustics, Aeroacoustics and Vibrations” Metadata:
- Title: ➤ Acoustics, Aeroacoustics and Vibrations
- Authors: Fabien AnselmetPierre-Olivier Mattei
- Language: English
- Number of Pages: Median: 528
- Publisher: ➤ Wiley & Sons, Incorporated, John
- Publish Date: 2016
“Acoustics, Aeroacoustics and Vibrations” Subjects and Themes:
- Subjects: ➤ Sound - Turbulence - Vibration - Aeroacoustics - TECHNOLOGY & ENGINEERING - Engineering (General) - Reference
Edition Identifiers:
- The Open Library ID: OL33536833M - OL28578471M - OL39908721M - OL29282424M
- Online Computer Library Center (OCLC) ID: 934513980
- All ISBNs: ➤ 9781848218611 - 1119178401 - 1848218613 - 9781119178408 - 9781119178361 - 1119178398 - 9781119178392 - 1119178363
Access and General Info:
- First Year Published: 2016
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Acoustics, Aeroacoustics and Vibrations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel
By Paul T. Soderman
“Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel” Metadata:
- Title: ➤ Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel
- Author: Paul T. Soderman
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va - [Washington, DC]
“Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel” Subjects and Themes:
- Subjects: Aeroacoustics - Design and construction - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL18035044M - OL21334944M - OL15299714M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Evaluation of a high-accuracy MacCormack type scheme using benchmark problems
By R. Hixon
“Evaluation of a high-accuracy MacCormack type scheme using benchmark problems” Metadata:
- Title: ➤ Evaluation of a high-accuracy MacCormack type scheme using benchmark problems
- Author: R. Hixon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Evaluation of a high-accuracy MacCormack type scheme using benchmark problems” Subjects and Themes:
- Subjects: Stability - Wavelengths - Aeroacoustics - Accuracy
Edition Identifiers:
- The Open Library ID: OL17543213M - OL15481366M - OL18112476M
- Online Computer Library Center (OCLC) ID: 38893842
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Evaluation of a high-accuracy MacCormack type scheme using benchmark problems at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Numerical simulation of the effect of heating on supersonic jet noise
By R. Hixon
“Numerical simulation of the effect of heating on supersonic jet noise” Metadata:
- Title: ➤ Numerical simulation of the effect of heating on supersonic jet noise
- Author: R. Hixon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Numerical simulation of the effect of heating on supersonic jet noise” Subjects and Themes:
- Subjects: ➤ Numerical analysis - Aeroacoustics - Computerized simulation - Sound generators - Sound propagation - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL17697880M - OL18121940M - OL17837373M
- Online Computer Library Center (OCLC) ID: 40128353
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of the effect of heating on supersonic jet noise at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Evaluation of a doubly-swept blade tip for rotorcraft noise reduction
By Brian E. Wake
“Evaluation of a doubly-swept blade tip for rotorcraft noise reduction” Metadata:
- Title: ➤ Evaluation of a doubly-swept blade tip for rotorcraft noise reduction
- Author: Brian E. Wake
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: [Springfield, Va - Hampton, Va
“Evaluation of a doubly-swept blade tip for rotorcraft noise reduction” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aeroacoustics - Blade tips - Blade slap noise - Aircraft noise - Sweep effect - Rotary wing aircraft - Blade-vortex interaction - Noise reduction - Euler equations of motion - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL15413638M - OL18081154M - OL17017557M
- Online Computer Library Center (OCLC) ID: 33411839
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Evaluation of a doubly-swept blade tip for rotorcraft noise reduction at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Ultra-high bypass ratio jet noise
By Low, John, K. C.
“Ultra-high bypass ratio jet noise” Metadata:
- Title: ➤ Ultra-high bypass ratio jet noise
- Author: Low, John, K. C.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Ultra-high bypass ratio jet noise” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Exhaust nozzles - Wind tunnel tests - Nozzle geometry - Subsonic speed - Bypass ratio - Noise intensity - Noise prediction (Aircraft) - Noise reduction - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL17683438M - OL17005197M - OL18078597M
- Online Computer Library Center (OCLC) ID: 32662654
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Ultra-high bypass ratio jet noise at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Inhomogeneous radiation boundary conditions simulating incoming acoustic waves for computational aeroacoustics
By Christopher K. W. Tam
“Inhomogeneous radiation boundary conditions simulating incoming acoustic waves for computational aeroacoustics” Metadata:
- Title: ➤ Inhomogeneous radiation boundary conditions simulating incoming acoustic waves for computational aeroacoustics
- Author: Christopher K. W. Tam
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Inhomogeneous radiation boundary conditions simulating incoming acoustic waves for computational aeroacoustics” Subjects and Themes:
- Subjects: Aeroacoustics - Boundary conditions - Finite difference theory - Sound waves - Wave propagation
Edition Identifiers:
- The Open Library ID: OL17697944M - OL17129412M - OL17593591M
- Online Computer Library Center (OCLC) ID: 40996906
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Inhomogeneous radiation boundary conditions simulating incoming acoustic waves for computational aeroacoustics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Time-domain impedance boundary conditions for computational aeroacoustics
By Christopher K. W. Tam
“Time-domain impedance boundary conditions for computational aeroacoustics” Metadata:
- Title: ➤ Time-domain impedance boundary conditions for computational aeroacoustics
- Author: Christopher K. W. Tam
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Washington, DC - Springfield, Va
“Time-domain impedance boundary conditions for computational aeroacoustics” Subjects and Themes:
- Subjects: Acoustic impedance - Aeroacoustics - Boundary conditions
Edition Identifiers:
- The Open Library ID: OL17556604M - OL18117399M - OL17124432M
- Online Computer Library Center (OCLC) ID: 39481800
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Time-domain impedance boundary conditions for computational aeroacoustics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Quiet high-speed fan
By Lysbeth Lieber
“Quiet high-speed fan” Metadata:
- Title: Quiet high-speed fan
- Author: Lysbeth Lieber
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Quiet high-speed fan” Subjects and Themes:
- Subjects: Aeroacoustics - Noise prediction - Turbofans - Engine noise - Noise reduction
Edition Identifiers:
- The Open Library ID: OL17593522M - OL18121546M - OL15505214M
- Online Computer Library Center (OCLC) ID: 41132219
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Quiet high-speed fan at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments
By M. A. Takallu
“Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments” Metadata:
- Title: ➤ Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments
- Author: M. A. Takallu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Reston, Va - Springfield, Va - [Washington, DC
“Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aeroacoustics - Computerized simulation - Reynolds averaging - Navier-Stokes equation - Aircraft noise - Aerodynamic noise - Flow visualization - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL15547652M - OL17591808M - OL18134640M
- Online Computer Library Center (OCLC) ID: 42666019
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Reynolds-averaged Navier-Stokes simulations of two partial-span flap wing experiments at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19A parallel compact multi-dimensional numerical algorithm with aeroacoustics applications
By Alex Povitsky
“A parallel compact multi-dimensional numerical algorithm with aeroacoustics applications” Metadata:
- Title: ➤ A parallel compact multi-dimensional numerical algorithm with aeroacoustics applications
- Author: Alex Povitsky
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“A parallel compact multi-dimensional numerical algorithm with aeroacoustics applications” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Algorithms - Computerized simulation - Parallel processing (Computers) - Turbulence - Wave propagation
Edition Identifiers:
- The Open Library ID: OL15559417M - OL18138513M - OL17592149M
- Online Computer Library Center (OCLC) ID: 43209327
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A parallel compact multi-dimensional numerical algorithm with aeroacoustics applications at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20Numerical simulation of the generation of axisymmetric mode jet screech tones
By Hao Shen
“Numerical simulation of the generation of axisymmetric mode jet screech tones” Metadata:
- Title: ➤ Numerical simulation of the generation of axisymmetric mode jet screech tones
- Author: Hao Shen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - Reston, Va - [Washington, DC
“Numerical simulation of the generation of axisymmetric mode jet screech tones” Subjects and Themes:
- Subjects: ➤ Screech tones - Axial flow - Aeroacoustics - Computerized simulation - Supersonic jet flow - Numerical flow visualization - Mach number - Axial compression loads
Edition Identifiers:
- The Open Library ID: OL17583550M - OL17701237M - OL18134632M
- Online Computer Library Center (OCLC) ID: 41639807
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Numerical simulation of the generation of axisymmetric mode jet screech tones at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Aeroacoustics of Low Mach Number Flows
By William Devenport and Stewart Glegg
“Aeroacoustics of Low Mach Number Flows” Metadata:
- Title: ➤ Aeroacoustics of Low Mach Number Flows
- Authors: William DevenportStewart Glegg
- Language: English
- Number of Pages: Median: 552
- Publisher: ➤ Elsevier Science & Technology - Elsevier Science & Technology Books
- Publish Date: 2017 - 2023
“Aeroacoustics of Low Mach Number Flows” Subjects and Themes:
- Subjects: ➤ Wind turbines - Aeroacoustics - Mach number - Aerodynamic noise - Aerodynamics - Mathematical models - Aérodynamique - Modèles mathématiques - Aéroacoustique - Nombre de Mach - Bruit aérodynamique - SCIENCE - Acoustics & Sound
Edition Identifiers:
- The Open Library ID: OL28624958M - OL49263678M - OL34531624M
- Online Computer Library Center (OCLC) ID: 973396718
- Library of Congress Control Number (LCCN): 2016962974
- All ISBNs: ➤ 9780128096512 - 0128097930 - 0443191123 - 9780128097939 - 0128096519 - 9780443191121
Access and General Info:
- First Year Published: 2017
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Aeroacoustics of Low Mach Number Flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
By Kenneth J. Baumeister
“Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow” Metadata:
- Title: ➤ Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
- Author: Kenneth J. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft engines - Ducted flow - Engine inlets - Finite difference theory - Iterative solution - Real time operation - Sound propagation
Edition Identifiers:
- The Open Library ID: OL17565459M - OL15497519M - OL18118423M
- Online Computer Library Center (OCLC) ID: 39725963
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
By Oktay Baysal
“Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization” Metadata:
- Title: ➤ Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
- Author: Oktay Baysal
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - Norfolk, Va
“Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic characteristics - Airfoils - Cavity flow - Computational fluid dynamics - Partial Differential equations - Unstructured grids (Mathematics)
Edition Identifiers:
- The Open Library ID: OL17796518M - OL15423196M
- Online Computer Library Center (OCLC) ID: 35268604
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24Comparison of the aeroacoustics of two small-scale supersonic inlets
By Wing Ng
“Comparison of the aeroacoustics of two small-scale supersonic inlets” Metadata:
- Title: ➤ Comparison of the aeroacoustics of two small-scale supersonic inlets
- Author: Wing Ng
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Comparison of the aeroacoustics of two small-scale supersonic inlets” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aircraft engines - Engine inlets - Flow distribution - Flow measurement - Inlet flow - Mach number - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL17593732M - OL15508989M
- Online Computer Library Center (OCLC) ID: 41272155
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Comparison of the aeroacoustics of two small-scale supersonic inlets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25The use of Kirchhoff's method in jet aeroacoustics
By Anastasios S. Lyrintzis
“The use of Kirchhoff's method in jet aeroacoustics” Metadata:
- Title: ➤ The use of Kirchhoff's method in jet aeroacoustics
- Author: Anastasios S. Lyrintzis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The use of Kirchhoff's method in jet aeroacoustics” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Computerized simulation - Far fields - Jet aircraft noise - Large eddy simulation - Supersonic jet flow
Edition Identifiers:
- The Open Library ID: OL15548313M - OL17839446M
- Online Computer Library Center (OCLC) ID: 41942475
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The use of Kirchhoff's method in jet aeroacoustics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26The Kirchhoff formulas for moving surfaces in aeroacoustics
By F. Farassat
“The Kirchhoff formulas for moving surfaces in aeroacoustics” Metadata:
- Title: ➤ The Kirchhoff formulas for moving surfaces in aeroacoustics
- Author: F. Farassat
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“The Kirchhoff formulas for moving surfaces in aeroacoustics” Subjects and Themes:
- Subjects: ➤ Kirchhoff law - Aeroacoustics - Noise prediction - Supersonic flow - Electromagnetism - Subsonic speed - Pipe flow
Edition Identifiers:
- The Open Library ID: OL17807035M - OL15482768M
- Online Computer Library Center (OCLC) ID: 37955730
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The Kirchhoff formulas for moving surfaces in aeroacoustics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27Nozzle thrust optimization while reducing jet noise
By John M. Seiner
“Nozzle thrust optimization while reducing jet noise” Metadata:
- Title: ➤ Nozzle thrust optimization while reducing jet noise
- Author: John M. Seiner
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Nozzle thrust optimization while reducing jet noise” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Convergent-divergent nozzles - Jet aircraft noise - Noise reduction - Nozzle design - Thrust augmentation
Edition Identifiers:
- The Open Library ID: OL15501903M - OL17595873M
- Online Computer Library Center (OCLC) ID: 42787303
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Nozzle thrust optimization while reducing jet noise at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer
By Meelan Choudhari
“Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer” Metadata:
- Title: ➤ Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer
- Author: Meelan Choudhari
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Boundary layer control - Boundary layer flow - Boundary layer stability - Compressible boundary layer - Suction - Two dimensional boundary layer
Edition Identifiers:
- The Open Library ID: OL17790197M - OL15403184M
- Online Computer Library Center (OCLC) ID: 32188843
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Effect of nonzero surface admittance on receptivity and stability of compressible boundary layer at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets
By James W. Russell
“Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Metadata:
- Title: ➤ Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets
- Author: James W. Russell
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic noise - Prediction analysis techniques - Acoustic frequencies - Jet mixing flow - Cold flow tests
Edition Identifiers:
- The Open Library ID: OL15564691M - OL17594107M
- Online Computer Library Center (OCLC) ID: 43837123
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Review of combustion-acoustic instabilities
By Ayo Oyediran
“Review of combustion-acoustic instabilities” Metadata:
- Title: ➤ Review of combustion-acoustic instabilities
- Author: Ayo Oyediran
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Review of combustion-acoustic instabilities” Subjects and Themes:
- Subjects: ➤ Combustion physics - Heat transfer - Aeroacoustics - Boundary conditions - Combustion stability - General overviews
Edition Identifiers:
- The Open Library ID: OL17116932M - OL17087720M
- Online Computer Library Center (OCLC) ID: 34616425
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Review of combustion-acoustic instabilities at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff
By Steven James Massey
“Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff” Metadata:
- Title: ➤ Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff
- Author: Steven James Massey
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2001
- Publish Location: Hanover, MD - Hampton, Va
“Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Analysis (Mathematics) - Aeroacoustics - Plug nozzles - Noise prediction - Flux difference splitting - Finite volume method
Edition Identifiers:
- The Open Library ID: OL17621406M - OL16042363M
- Online Computer Library Center (OCLC) ID: 54502332
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Computational analyses of propulsion aeroacoustics for mixed flow nozzle pylon installation at takeoff at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32Review of combustion-acoustic instabilities
By Abraham Ayowole Oyediran
“Review of combustion-acoustic instabilities” Metadata:
- Title: ➤ Review of combustion-acoustic instabilities
- Author: Abraham Ayowole Oyediran
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Review of combustion-acoustic instabilities” Subjects and Themes:
- Subjects: ➤ Combustion physics - Heat transfer - Aeroacoustics - Boundary conditions - Combustion stability - General overviews
Edition Identifiers:
- The Open Library ID: OL18085514M - OL15420737M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Review of combustion-acoustic instabilities at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33Investigation of dispersion-relation-preserving scheme and spectral analysis methods for acoustic waves
By Florence O. Vanel
“Investigation of dispersion-relation-preserving scheme and spectral analysis methods for acoustic waves” Metadata:
- Title: ➤ Investigation of dispersion-relation-preserving scheme and spectral analysis methods for acoustic waves
- Author: Florence O. Vanel
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Investigation of dispersion-relation-preserving scheme and spectral analysis methods for acoustic waves” Subjects and Themes:
- Subjects: ➤ Wave dispersion - Aeroacoustics - Average - Weighting functions - Algorithms - Wave propagation - Boundary conditions - Sound waves - Two dimensional models - Spectral methods
Edition Identifiers:
- The Open Library ID: OL17794098M - OL15419539M
- Online Computer Library Center (OCLC) ID: 34600919
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Investigation of dispersion-relation-preserving scheme and spectral analysis methods for acoustic waves at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34Continued development of the discontinuous Galerkin method for computational aeroacoustic applications
By H. L. Atkins
“Continued development of the discontinuous Galerkin method for computational aeroacoustic applications” Metadata:
- Title: ➤ Continued development of the discontinuous Galerkin method for computational aeroacoustic applications
- Author: H. L. Atkins
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Reston, VA - [Washington, DC - Springfield, Va
“Continued development of the discontinuous Galerkin method for computational aeroacoustic applications” Subjects and Themes:
- Subjects: Aeroacoustics - Boundary conditions - Differential equations - Quadratures - Walls
Edition Identifiers:
- The Open Library ID: OL17592991M - OL15543073M
- Online Computer Library Center (OCLC) ID: 41264507
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Continued development of the discontinuous Galerkin method for computational aeroacoustic applications at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35The aeroacoustics of supersonic coaxial jets
By Milo D. Dahl
“The aeroacoustics of supersonic coaxial jets” Metadata:
- Title: ➤ The aeroacoustics of supersonic coaxial jets
- Author: Milo D. Dahl
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“The aeroacoustics of supersonic coaxial jets” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Coaxial flow - Gas jets - Jet aircraft noise - Noise prediction (Aircraft) - Noise reduction - Supersonic jet flow
Edition Identifiers:
- The Open Library ID: OL17788449M - OL15408592M
- Online Computer Library Center (OCLC) ID: 32668885
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The aeroacoustics of supersonic coaxial jets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Supersonic coaxial jet noise predictions
By Milo D. Dahl
“Supersonic coaxial jet noise predictions” Metadata:
- Title: ➤ Supersonic coaxial jet noise predictions
- Author: Milo D. Dahl
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Supersonic coaxial jet noise predictions” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Mixing length flow theory - Turbulence models - Supersonic jet flow - Coaxial flow - Noise prediction (Aircraft) - Noise reduction - Aeroacoustics - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15413486M - OL17791557M
- Online Computer Library Center (OCLC) ID: 33441989
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Supersonic coaxial jet noise predictions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37Computing axisymmetric jet screech tones using unstructured grids
By Philip C. E. Jorgenson
“Computing axisymmetric jet screech tones using unstructured grids” Metadata:
- Title: ➤ Computing axisymmetric jet screech tones using unstructured grids
- Author: Philip C. E. Jorgenson
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
- Publish Date: 2002
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio] - Springfield, VA
“Computing axisymmetric jet screech tones using unstructured grids” Subjects and Themes:
- Subjects: Aeroacoustics - Axisymmetric flow - Nozzle geometry - Screech tones - Unstructured grids
Edition Identifiers:
- The Open Library ID: OL17634848M - OL16098758M
- Online Computer Library Center (OCLC) ID: 57252947
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Computing axisymmetric jet screech tones using unstructured grids at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38Quelling cabin noise in turboprop aircraft via active control
By Rex K. Kincaid
“Quelling cabin noise in turboprop aircraft via active control” Metadata:
- Title: ➤ Quelling cabin noise in turboprop aircraft via active control
- Author: Rex K. Kincaid
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Quelling cabin noise in turboprop aircraft via active control” Subjects and Themes:
- Subjects: ➤ Noise intensity - Aeroacoustics - Noise reduction - Vibration - Actuators - Jet aircraft noise - Active control
Edition Identifiers:
- The Open Library ID: OL15508979M - OL17593730M
- Online Computer Library Center (OCLC) ID: 40929309
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Quelling cabin noise in turboprop aircraft via active control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39Computation of noise radiation from turbofans
By M. Nallasamy
“Computation of noise radiation from turbofans” Metadata:
- Title: ➤ Computation of noise radiation from turbofans
- Author: M. Nallasamy
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C.?] - [Springfield, Va
“Computation of noise radiation from turbofans” Subjects and Themes:
- Subjects: ➤ Turbofans - Far fields - Air ducts - Noise prediction (Aircraft) - Aerodynamic noise - Turbofan engines - Aeroacoustics - Engine noise - Jet aircraft noise - Finite element method
Edition Identifiers:
- The Open Library ID: OL17794640M - OL17684879M
- Online Computer Library Center (OCLC) ID: 34702918
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Computation of noise radiation from turbofans at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
40The acoustics of a lined duct with flow
By S. W. Rienstra
“The acoustics of a lined duct with flow” Metadata:
- Title: ➤ The acoustics of a lined duct with flow
- Author: S. W. Rienstra
- Publisher: National Aerospace Laboratory
- Publish Date: 1987
- Publish Location: Amsterdam
“The acoustics of a lined duct with flow” Subjects and Themes:
- Subjects: ➤ Acoustic ducts - Aeroacoustics - Acoustic impedance - Humanities - Religion & beliefs - History
Edition Identifiers:
- The Open Library ID: OL20898853M
- All ISBNs: 69
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The acoustics of a lined duct with flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
41Suppression of refraction in jet noise by cooling
By J. T. Kelsall
“Suppression of refraction in jet noise by cooling” Metadata:
- Title: ➤ Suppression of refraction in jet noise by cooling
- Author: J. T. Kelsall
- Number of Pages: Median: 12
- Publisher: ➤ Dept. of Aerospace Science and Engineering - Institute for Aerospace Studies
- Publish Date: 1975
- Publish Location: [Downsview, Ont.]
“Suppression of refraction in jet noise by cooling” Subjects and Themes:
- Subjects: Refraction - Jet flow - Aeroacoustics - Noise (Sound) - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL20899472M - OL19988132M
Access and General Info:
- First Year Published: 1975
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Suppression of refraction in jet noise by cooling at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
42The research and training activities for the Joint Institute for Aeronautics and Acoustics
By Brian Cantwell
“The research and training activities for the Joint Institute for Aeronautics and Acoustics” Metadata:
- Title: ➤ The research and training activities for the Joint Institute for Aeronautics and Acoustics
- Author: Brian Cantwell
- Language: English
- Publisher: ➤ The Institute - National Technical Information Service, distributor - National Aeronautics and Space Administration - NASA-Ames Stanford University, Joint Institute for Aeronautics and Acoustics
- Publish Date: 1996 - 1997
- Publish Location: ➤ [Stanford, Calif.] - [Washington, DC - [Sanford, Calif.] - Springfield, Va
“The research and training activities for the Joint Institute for Aeronautics and Acoustics” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Computational fluid dynamics - Control simulation - University program - Aerodynamics - Research - Education - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15539633M - OL15543239M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The research and training activities for the Joint Institute for Aeronautics and Acoustics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
43Noise impact of advanced high lift systems
By Kevin R. Elmer
“Noise impact of advanced high lift systems” Metadata:
- Title: ➤ Noise impact of advanced high lift systems
- Author: Kevin R. Elmer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Noise impact of advanced high lift systems” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic noise - Aircraft design - Engine noise - Jet aircraft noise - Lift - Noise reduction - Passenger aircraft - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15416073M - OL17791319M
- Online Computer Library Center (OCLC) ID: 33241385
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Noise impact of advanced high lift systems at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
44Coupling of low speed fan stator vane unsteady pressures to duct modes
By Daniel L. Sutliff
“Coupling of low speed fan stator vane unsteady pressures to duct modes” Metadata:
- Title: ➤ Coupling of low speed fan stator vane unsteady pressures to duct modes
- Author: Daniel L. Sutliff
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio]
“Coupling of low speed fan stator vane unsteady pressures to duct modes” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Noise intensity - Pressure distribution - Predictions - Ducted fans - Aircraft noise - Rotor stator interactions - Engine noise - Green's functions
Edition Identifiers:
- The Open Library ID: OL15550581M - OL17584189M
- Online Computer Library Center (OCLC) ID: 42333114
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Coupling of low speed fan stator vane unsteady pressures to duct modes at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
45Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report
By Joseph R. Hauser
“Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report” Metadata:
- Title: ➤ Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report
- Author: Joseph R. Hauser
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Bypass ratio - Engine noise - Jet aircraft noise - Noise reduction - Subsonic flow
Edition Identifiers:
- The Open Library ID: OL16031810M - OL17604935M
- Online Computer Library Center (OCLC) ID: 49946276
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
46Acoustic and aerodynamic study of a pusher-propeller aircraft model
By Paul T. Soderman
“Acoustic and aerodynamic study of a pusher-propeller aircraft model” Metadata:
- Title: ➤ Acoustic and aerodynamic study of a pusher-propeller aircraft model
- Author: Paul T. Soderman
- Language: English
- Number of Pages: Median: 59
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Acoustic and aerodynamic study of a pusher-propeller aircraft model” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Aeroacoustics - Aircraft models - Aircraft wakes - Interactional aerodynamics - Noise - Propeller blades - Propeller noise - Wakes (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16135237M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Acoustic and aerodynamic study of a pusher-propeller aircraft model at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
47Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight
By R. Martinez
“Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight” Metadata:
- Title: ➤ Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight
- Author: R. Martinez
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Diffraction - Diffraction patterns - Dissipation - Ducts - Propeller noise - Ring wings - Shrouded propellers
Edition Identifiers:
- The Open Library ID: OL15409343M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
48Aerodynamics and aeroacoustics of rotorcraft
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Aerodynamics and aeroacoustics of rotorcraft” Metadata:
- Title: ➤ Aerodynamics and aeroacoustics of rotorcraft
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Number of Pages: Median: 508
- Publisher: AGARD
- Publish Date: 1995
- Publish Location: Neuilly sur Seine, France
“Aerodynamics and aeroacoustics of rotorcraft” Subjects and Themes:
- Subjects: Aeroacoustics - Aerodynamics - Helicopters - Rotary wing aircraft
Edition Identifiers:
- The Open Library ID: OL19004289M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Aerodynamics and aeroacoustics of rotorcraft at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
49Assessment of NASA's aircraft noise prediction capability
By Milo D. Dahl
“Assessment of NASA's aircraft noise prediction capability” Metadata:
- Title: ➤ Assessment of NASA's aircraft noise prediction capability
- Author: Milo D. Dahl
- Language: English
- Number of Pages: Median: 354
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2012
- Publish Location: Cleveland, Ohio
“Assessment of NASA's aircraft noise prediction capability” Subjects and Themes:
- Subjects: ➤ Jet planes - Noise - Aeroacoustics - Noise prediction (aircraft) - Jet aircraft noise - Wind tunnel tests - Hypersonic aircraft - Subsonic aircraft - Rotary wing aircraft - Computational fluid dynamics - Aircraft noise - Supersonic aircraft
Edition Identifiers:
- The Open Library ID: OL31033961M
- Online Computer Library Center (OCLC) ID: 818645984 - 823318882
- Library of Congress Control Number (LCCN): 2012515605
Access and General Info:
- First Year Published: 2012
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Assessment of NASA's aircraft noise prediction capability at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
50Separate flow nozzle test status meeting
“Separate flow nozzle test status meeting” Metadata:
- Title: ➤ Separate flow nozzle test status meeting
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 2000
- Publish Location: [Washington, DC] - Hanover, MD
“Separate flow nozzle test status meeting” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Sonic nozzles - Exhaust nozzles - Engine noise - Jet aircraft noise - Acoustic nozzles
Edition Identifiers:
- The Open Library ID: OL14524905M
- Online Computer Library Center (OCLC) ID: 50769127
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Separate flow nozzle test status meeting at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.