Explore: Axisymmetric Flow
Discover books, insights, and more — all in one place.
Learn more about Axisymmetric Flow with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “axisymmetric-flow”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors
By James F. Schmidt
“Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors” Metadata:
- Title: ➤ Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors
- Author: James F. Schmidt
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Axial flow - Axisymmetric flow - Performance prediction - Rotor aerodynamics - Steady flow - Turbocompressors - Turbofans - User manuals (Computer programs)
Edition Identifiers:
- The Open Library ID: OL17107865M - OL18086876M - OL15423145M
- Online Computer Library Center (OCLC) ID: 35248220
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 Off-design computer code for calculating the aerodynamic performance of axial-flow fans and compressors at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Self-similar compressible free vortices
By Karl Von Ellenrieder
“Self-similar compressible free vortices” Metadata:
- Title: ➤ Self-similar compressible free vortices
- Author: Karl Von Ellenrieder
- Language: English
- Publisher: ➤ Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - [Stanford, Calif.]
“Self-similar compressible free vortices” Subjects and Themes:
- Subjects: ➤ Lie groups - Numerical analysis - Perturbation - Vorticity - Vortices - Mathematical models - Two dimensional flow - Axisymmetric flow - Prandtl number - Navier-Stokes equation - Incompressible flow - Free flow
Edition Identifiers:
- The Open Library ID: OL17581926M - OL15545013M - OL17131181M - OL18133565M
- Online Computer Library Center (OCLC) ID: 41414290
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 Self-similar compressible free vortices at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Axisymmetric free shear flows with and without swirl
By Alan Peter Morse
“Axisymmetric free shear flows with and without swirl” Metadata:
- Title: ➤ Axisymmetric free shear flows with and without swirl
- Author: Alan Peter Morse
- Language: English
- Number of Pages: Median: 533
- Publisher: ➤ Mechanical Engineering Dept., Imperial College of Science and Technology - University of London, Faculty of Engineering
- Publish Date: 1980
- Publish Location: London
“Axisymmetric free shear flows with and without swirl” Subjects and Themes:
- Subjects: Axisymmetric flow - Swirling - Swirling flows - Shear flow
Edition Identifiers:
- The Open Library ID: OL49981121M - OL18930386M - OL19917074M
- Online Computer Library Center (OCLC) ID: 76955598
Access and General Info:
- First Year Published: 1980
- 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 Axisymmetric free shear flows with and without swirl at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique
By J. K. Ahuja
“Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique” Metadata:
- Title: ➤ Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique
- Author: J. K. Ahuja
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautiacs - Old Dominion University Research Foundation
- Publish Date: 1994
- Publish Location: ➤ Washington, D. C - Springfield, Va - Norfolk, Va - [Washington, DC
“Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique” Subjects and Themes:
- Subjects: ➤ Viscous flow - Axisymmetric flow - Combustible flow - Hypersonic combustion - Hydrogen - Shock fitting - Projectiles - Blunt bodies - Shock-induced combustion - Gas mixtures - Bow waves - Shock layers - Shock waves
Edition Identifiers:
- The Open Library ID: OL22346979M - OL15408736M - OL17788521M
- Online Computer Library Center (OCLC) ID: 32677297
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 Numerical simulation of shock-induced combustion past blunt bodies using shock-fitting technique at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Numerical investigations in the backflow region of a vacuum plume
By G. S. Liaw
“Numerical investigations in the backflow region of a vacuum plume” Metadata:
- Title: ➤ Numerical investigations in the backflow region of a vacuum plume
- Author: G. S. Liaw
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Alabama A&M University - National Aeronautics and Space Administration
- Publish Date: 1992 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Normal, Ala
“Numerical investigations in the backflow region of a vacuum plume” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Boltzmann transport equation - Rocket exhaust - Space vehicles - Rarefied gases - Nozzle flow - Plumes - Plumes (Fluid dynamics) - Axisymmetric flow - Propulsion systems - Low density flow - Computer programs - Finite difference theory - Flow distribution - Monte Carlo method - Gas flow
Edition Identifiers:
- The Open Library ID: OL15419030M - OL15367145M
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 Numerical investigations in the backflow region of a vacuum plume at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Enhanced mixing of an axisymmetric jet by aerodynamic excitation
By Ganesh Raman
“Enhanced mixing of an axisymmetric jet by aerodynamic excitation” Metadata:
- Title: ➤ Enhanced mixing of an axisymmetric jet by aerodynamic excitation
- Author: Ganesh Raman
- Language: English
- Number of Pages: Median: 170
- Publisher: ➤ Lewis Research Center - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va
“Enhanced mixing of an axisymmetric jet by aerodynamic excitation” Subjects and Themes:
- Subjects: ➤ Fluid dynamics - Jets - Axisymmetric flow - Shear layers - Vortices - Surface noise interactions - Mixing - Acoustic excitation
Edition Identifiers:
- The Open Library ID: OL17684161M - OL14984741M
Access and General Info:
- First Year Published: 1986
- 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 Enhanced mixing of an axisymmetric jet by aerodynamic excitation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Computing 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.
8Computer program BL2D for solving two-dimensional and axisymmetric boundary layers
By Venkit Iyer
“Computer program BL2D for solving two-dimensional and axisymmetric boundary layers” Metadata:
- Title: ➤ Computer program BL2D for solving two-dimensional and axisymmetric boundary layers
- Author: Venkit Iyer
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, VA
“Computer program BL2D for solving two-dimensional and axisymmetric boundary layers” Subjects and Themes:
- Subjects: ➤ Applications programs (Computers) - Axisymmetric flow - Boundary layer flow - Computational fluid dynamics - Two dimensional boundary layer - User manuals (Computer programs)
Edition Identifiers:
- The Open Library ID: OL17791631M - OL15413623M
- Online Computer Library Center (OCLC) ID: 34140060
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Computer program BL2D for solving two-dimensional and axisymmetric boundary layers at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions
By Y. Y. Chan
“Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions” Metadata:
- Title: ➤ Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions
- Author: Y. Y. Chan
- Number of Pages: Median: 49
- Publisher: ➤ Institute for Aerospace Studies - [Institute for Aerospace Studies]
- Publish Date: 1965
- Publish Location: [Downsview, Ont.]
“Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions” Subjects and Themes:
- Subjects: Axisymmetric flow - Compressible boundary layer - Hypersonic flow - Laminar boundary flow - Laminar boundary layer
Edition Identifiers:
- The Open Library ID: OL20897787M - OL20986487M
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Integral methods in compressible laminar boundary layers and their application to hypersonic pressure interactions at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Calculations of diffuser flows with an anisotropic K-[epsilon] model
By Jiang Zhu
“Calculations of diffuser flows with an anisotropic K-[epsilon] model” Metadata:
- Title: ➤ Calculations of diffuser flows with an anisotropic K-[epsilon] model
- Author: Jiang Zhu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Calculations of diffuser flows with an anisotropic K-[epsilon] model” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Computational fluid dynamics - Computational grids - Finite element method - Grid generation (Mathematics) - Incompressible flow - Internal flow - K-epsilon turbulence model - Navier-Stokes equation - Stress-strain relationships
Edition Identifiers:
- The Open Library ID: OL17117660M
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 Calculations of diffuser flows with an anisotropic K-[epsilon] model at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Three component laser Doppler measurements in an axisymmetric jet
By John M. Kuhlman
“Three component laser Doppler measurements in an axisymmetric jet” Metadata:
- Title: ➤ Three component laser Doppler measurements in an axisymmetric jet
- Author: John M. Kuhlman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Three component laser Doppler measurements in an axisymmetric jet” Subjects and Themes:
- Subjects: Axisymmetric flow - Fluid jets - Laser Doppler velocimeters - Three dimensional flow - Velocity measurement
Edition Identifiers:
- The Open Library ID: OL16121106M
Access and General Info:
- First Year Published: 1989
- 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 Three component laser Doppler measurements in an axisymmetric jet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Experimental study of vortex breakdown in a cylindrical, swirling flow
“Experimental study of vortex breakdown in a cylindrical, swirling flow” Metadata:
- Title: ➤ Experimental study of vortex breakdown in a cylindrical, swirling flow
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Stanford, Calif.] - [Washington, DC
“Experimental study of vortex breakdown in a cylindrical, swirling flow” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Vortex breakdown - Reynolds number - Steady flow - Flow stability - Cylindrical bodies - Swirling - Internal flow - Aspect ratio
Edition Identifiers:
- The Open Library ID: OL17838001M
- Online Computer Library Center (OCLC) ID: 40101976
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 Experimental study of vortex breakdown in a cylindrical, swirling flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13On the conditions for resonance interactions of instability waves in the axisymmetric jet
By Reda R. Mankbadi
“On the conditions for resonance interactions of instability waves in the axisymmetric jet” Metadata:
- Title: ➤ On the conditions for resonance interactions of instability waves in the axisymmetric jet
- Author: Reda R. Mankbadi
- Number of Pages: Median: 11
- Publisher: ICOMP
- Publish Date: 1989
- Publish Location: Cleveland, Ohio
“On the conditions for resonance interactions of instability waves in the axisymmetric jet” Subjects and Themes:
- Subjects: Resonance - Axisymmetric flow
Edition Identifiers:
- The Open Library ID: OL18930970M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find On the conditions for resonance interactions of instability waves in the axisymmetric jet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Comparison of 3D computation and experiment for non-axisymmetric nozzles
By H. T. Lai
“Comparison of 3D computation and experiment for non-axisymmetric nozzles” Metadata:
- Title: ➤ Comparison of 3D computation and experiment for non-axisymmetric nozzles
- Author: H. T. Lai
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Comparison of 3D computation and experiment for non-axisymmetric nozzles” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axisymmetric flow - Three dimensional models - Supersonic flow - Nozzle design - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15407719M
Access and General Info:
- First Year Published: 1989
- 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 3D computation and experiment for non-axisymmetric nozzles at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15The flow induced by the coalescence of two initially stationary drops
By M. R. H. Nobari
“The flow induced by the coalescence of two initially stationary drops” Metadata:
- Title: ➤ The flow induced by the coalescence of two initially stationary drops
- Author: M. R. H. Nobari
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va
“The flow induced by the coalescence of two initially stationary drops” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axisymmetric flow - Finite difference theory - Unsteady flow - Fluid flow - Liquid-liquid interfaces - Viscosity - Drops (Liquids) - Navier-Stokes equation - Penetration - Interfacial tension - Coalescing
Edition Identifiers:
- The Open Library ID: OL15408170M
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 flow induced by the coalescence of two initially stationary drops at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Model of an aero-space plane based on an idealized cone-derived waverider forebody
By Hyung-Koo Park
“Model of an aero-space plane based on an idealized cone-derived waverider forebody” Metadata:
- Title: ➤ Model of an aero-space plane based on an idealized cone-derived waverider forebody
- Author: Hyung-Koo Park
- Number of Pages: Median: 146
- Publisher: University of Oklahoma
- Publish Date: 1990
- Publish Location: Norman, Okla
“Model of an aero-space plane based on an idealized cone-derived waverider forebody” Subjects and Themes:
- Subjects: Axisymmetric flow - Aerospace planes - Waveriders
Edition Identifiers:
- The Open Library ID: OL19244204M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Model of an aero-space plane based on an idealized cone-derived waverider forebody at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Rapid numerical simulation of viscous axisymmetric flow fields
By Daniel L. Tweedt
“Rapid numerical simulation of viscous axisymmetric flow fields” Metadata:
- Title: ➤ Rapid numerical simulation of viscous axisymmetric flow fields
- Author: Daniel L. Tweedt
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Rapid numerical simulation of viscous axisymmetric flow fields” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Axisymmetric flow - Pressure distribution - Transonic flow - Turbulence models - Finite difference theory - Navier-Stokes equation - Flow distribution - Runge-Kutta method - Shock waves
Edition Identifiers:
- The Open Library ID: OL15420864M
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 Rapid numerical simulation of viscous axisymmetric flow fields at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
By William B. Compton
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Metadata:
- Title: ➤ Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
- Author: William B. Compton
- 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
“Comparison of turbulence models for nozzle-afterbody flows with propulsive jets” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Angle of attack - Axisymmetric flow - Computational fluid dynamics - Convergent-divergent nozzles - Exhaust gases - Free flow - Jet exhaust - K-epsilon turbulence model - Navier-Stokes equation - Nozzle flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15504433M
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 turbulence models for nozzle-afterbody flows with propulsive jets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19An outflow boundary condition for aeroacoustic computations
By Ehteshamul Md Hayder
“An outflow boundary condition for aeroacoustic computations” Metadata:
- Title: ➤ An outflow boundary condition for aeroacoustic computations
- Author: Ehteshamul Md Hayder
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion
- Publish Date: 1995
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va
“An outflow boundary condition for aeroacoustic computations” Subjects and Themes:
- Subjects: Axisymmetric flow - Boundary conditions - Aeroacoustics - Computation - Jet flow
Edition Identifiers:
- The Open Library ID: OL15413499M
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 An outflow boundary condition for aeroacoustic computations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20The inviscid axisymmetric stability of the supersonic flow along a circular cylinder
By Peter W. Duck
“The inviscid axisymmetric stability of the supersonic flow along a circular cylinder” Metadata:
- Title: ➤ The inviscid axisymmetric stability of the supersonic flow along a circular cylinder
- Author: Peter W. Duck
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: [Springfield, Va - Hampton, VA
“The inviscid axisymmetric stability of the supersonic flow along a circular cylinder” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Circular cylinders - Boundary layer stability - Supersonic flow - Thin walled shells - Boundary layer flow
Edition Identifiers:
- The Open Library ID: OL15407988M
Access and General Info:
- First Year Published: 1989
- 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 inviscid axisymmetric stability of the supersonic flow along a circular cylinder at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows
By Peter W. Duck
“On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows” Metadata:
- Title: ➤ On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows
- Author: Peter W. Duck
- Number of Pages: Median: 18
- Publisher: ICASE
- Publish Date: 1988
- Publish Location: Hampton, Va
“On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows” Subjects and Themes:
- Subjects: Tollmien-Schlichting waves - Axisymmetric flow - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL20897994M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find On the interaction of Tollmien-Schlichting waves in axisymmetric supersonic flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
By George T. Carson
“Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” Metadata:
- Title: ➤ Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
- Author: George T. Carson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” Subjects and Themes:
- Subjects: ➤ Transonic wind tunnels - Axisymmetric flow - Thrust vector control - Wind tunnel tests - Nozzle design - Static tests - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15405712M
Access and General Info:
- First Year Published: 1991
- 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 Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23Supersonic jet noise reductions predicted with increased jet spreading rate
By Milo D. Dahl
“Supersonic jet noise reductions predicted with increased jet spreading rate” Metadata:
- Title: ➤ Supersonic jet noise reductions predicted with increased jet spreading rate
- 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, DC]
“Supersonic jet noise reductions predicted with increased jet spreading rate” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Aeroacoustics - Jet mixing flow - Mathematical models - Supersonic jet flow - Noise prediction (Aircraft) - Aerodynamic noise - Noise reduction - Engine noise - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15411414M
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 jet noise reductions predicted with increased jet spreading rate at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24Calculations of diffuser flows with an anisotropic K-[epsilon] model
By Chiang Chu
“Calculations of diffuser flows with an anisotropic K-[epsilon] model” Metadata:
- Title: ➤ Calculations of diffuser flows with an anisotropic K-[epsilon] model
- Author: Chiang Chu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Calculations of diffuser flows with an anisotropic K-[epsilon] model” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axisymmetric flow - Computational grids - Incompressible flow - Navier-Stokes equation - Internal flow - Grid generation (Mathematics) - Finite element method - K-epsilon turbulence model - Stress-strain relationships
Edition Identifiers:
- The Open Library ID: OL15426052M
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 Calculations of diffuser flows with an anisotropic K-[epsilon] model at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25Hydrodynamic calculations of axisymmetric accretion flow
By Eiji Shima
“Hydrodynamic calculations of axisymmetric accretion flow” Metadata:
- Title: ➤ Hydrodynamic calculations of axisymmetric accretion flow
- Author: Eiji Shima
- Number of Pages: Median: 20
- Publisher: ➤ Gasdynamics Laboratory, Dept. of Aeronautical Engineering, Faculty of Engineering, Kyoto University
- Publish Date: 1985
- Publish Location: Kyoto
“Hydrodynamic calculations of axisymmetric accretion flow” Subjects and Themes:
- Subjects: Axisymmetric flow
Edition Identifiers:
- The Open Library ID: OL19985801M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Hydrodynamic calculations of axisymmetric accretion flow at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26Studies of ion drift in axisymmetric flow fields
By David John Bruno Venturi
“Studies of ion drift in axisymmetric flow fields” Metadata:
- Title: ➤ Studies of ion drift in axisymmetric flow fields
- Author: David John Bruno Venturi
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1976
- Publish Location: [Downsview, Ont.]
“Studies of ion drift in axisymmetric flow fields” Subjects and Themes:
- Subjects: Ions - Axisymmetric flow
Edition Identifiers:
- The Open Library ID: OL19986424M
Access and General Info:
- First Year Published: 1976
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Studies of ion drift in axisymmetric flow fields at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27The design/analysis of flows through turbomachinery
By D. P. Miller
“The design/analysis of flows through turbomachinery” Metadata:
- Title: ➤ The design/analysis of flows through turbomachinery
- Author: D. P. Miller
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“The design/analysis of flows through turbomachinery” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Axisymmetric flow - Viscous flow - Rotor blades (Turbomachinery) - Applications programs (Computers) - Flow distribution - Grid generation (Mathematics) - Turbomachinery
Edition Identifiers:
- The Open Library ID: OL15417825M
Access and General Info:
- First Year Published: 1991
- 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 design/analysis of flows through turbomachinery at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Inlet flow test calibration for a small axial compressor rig
By D. P. Miller
“Inlet flow test calibration for a small axial compressor rig” Metadata:
- Title: ➤ Inlet flow test calibration for a small axial compressor rig
- Author: D. P. Miller
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Inlet flow test calibration for a small axial compressor rig” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axisymmetric flow - Test stands - Calibrating - Engine testing laboratories - Inlet flow - Turbocompressors
Edition Identifiers:
- The Open Library ID: OL15414468M
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 Inlet flow test calibration for a small axial compressor rig at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation
By Clinton P. T. Groth
“Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation” Metadata:
- Title: ➤ Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation
- Author: Clinton P. T. Groth
- Number of Pages: Median: 311
- Publisher: Pineridge
- Publish Date: 1991
- Publish Location: Swansea, U. K
“Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation” Subjects and Themes:
- Subjects: Axisymmetric flow - Turbulence models
Edition Identifiers:
- The Open Library ID: OL21499803M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Evaluation of scale evolution turbulence models for axisymmetric internal flows with separation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation
By Chin-Shun Lin
“Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation” Metadata:
- Title: ➤ Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation
- Author: Chin-Shun Lin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ Cleveland, Ohio - [Springfield, Va
“Numerical studies of the effects of jet-induced mixing on liquid-vapor interface condensation” Subjects and Themes:
- Subjects: Jet mixing flow - Mathematical models - Axisymmetric flow - Liquid-vapor interfaces - Condensing
Edition Identifiers:
- The Open Library ID: OL15408049M
Access and General Info:
- First Year Published: 1989
- 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 studies of the effects of jet-induced mixing on liquid-vapor interface condensation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
By Mary L. Mason
“Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Metadata:
- Title: ➤ Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
- Author: Mary L. Mason
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Pitching (Aerodynamics) - Thrust vector control - Motors - Nozzle geometry - Airplanes - Short takeoff aircraft - Short take-off and landing aircraft - Static tests - Testing - Nozzle thrust coefficients - Jet nozzles - Thrust
Edition Identifiers:
- The Open Library ID: OL16116664M
Access and General Info:
- First Year Published: 1986
- 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 Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32Numerical simulations of the flow in the HYPULSE expansion tube
By Gregory J. Wilson
“Numerical simulations of the flow in the HYPULSE expansion tube” Metadata:
- Title: ➤ Numerical simulations of the flow in the HYPULSE expansion tube
- Author: Gregory J. Wilson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Numerical simulations of the flow in the HYPULSE expansion tube” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Axisymmetric flow - Computerized simulation - Boundary layer flow - Turbulent boundary layer - Laminar flow - Flow distribution - Laminar boundary layer - Nitrogen - Shock tubes - Gas expansion
Edition Identifiers:
- The Open Library ID: OL15414550M
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 Numerical simulations of the flow in the HYPULSE expansion tube at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33The filtered Abel transform and its application in combustion diagnostics
By Zeng-Guang Yuan
“The filtered Abel transform and its application in combustion diagnostics” Metadata:
- Title: ➤ The filtered Abel transform and its application in combustion diagnostics
- Author: Zeng-Guang Yuan
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA - Hanover, MD
“The filtered Abel transform and its application in combustion diagnostics” Subjects and Themes:
- Subjects: ➤ Fourier transformation - Axisymmetric flow - Combustion - Diagnosis - Diffusion flames - Abel function - Kernel functions
Edition Identifiers:
- The Open Library ID: OL16094128M
Access and General Info:
- First Year Published: 2003
- 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 filtered Abel transform and its application in combustion diagnostics at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34Marangoni convection in a gravity-free silicon float zone
By Samuel Ohring
“Marangoni convection in a gravity-free silicon float zone” Metadata:
- Title: ➤ Marangoni convection in a gravity-free silicon float zone
- Author: Samuel Ohring
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Carderock Division, Naval Surface Warfare Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Bethesda, Md - Springfield, Va - [Washington, DC
“Marangoni convection in a gravity-free silicon float zone” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Axisymmetric flow - Marangoni convection - Float zones - Time dependence - Heat transfer - Navier-Stokes equation - Silicon - Microgravity
Edition Identifiers:
- The Open Library ID: OL15410002M
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 Marangoni convection in a gravity-free silicon float zone at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35Spreading characteristics and thrust of jets from asymmetric nozzles
By K. B. M. O. Zaman
“Spreading characteristics and thrust of jets from asymmetric nozzles” Metadata:
- Title: ➤ Spreading characteristics and thrust of jets from asymmetric nozzles
- Author: K. B. M. O. Zaman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Spreading characteristics and thrust of jets from asymmetric nozzles” Subjects and Themes:
- Subjects: ➤ Asymmetry - Axisymmetric flow - Nozzle flow - Sound pressure - Spreading - Tabs (Control surfaces) - Vortices
Edition Identifiers:
- The Open Library ID: OL15423294M
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 Spreading characteristics and thrust of jets from asymmetric nozzles at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Computations of axisymmetric flows in hypersonic shock tubes
By Surendra P. Sharma
“Computations of axisymmetric flows in hypersonic shock tubes” Metadata:
- Title: ➤ Computations of axisymmetric flows in hypersonic shock tubes
- Author: Surendra P. Sharma
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - [National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Washington, DC
“Computations of axisymmetric flows in hypersonic shock tubes” Subjects and Themes:
- Subjects: Computational fluid dynamics - Axisymmetric flow - Flow distribution - Supersonic speed - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15539928M
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 Computations of axisymmetric flows in hypersonic shock tubes at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37Jets and flames in co-flowing streams
By S. Ha
“Jets and flames in co-flowing streams” Metadata:
- Title: ➤ Jets and flames in co-flowing streams
- Author: S. Ha
- Publisher: AIAA
- Publish Date: 1987
- Publish Location: New York
“Jets and flames in co-flowing streams” Subjects and Themes:
- Subjects: Axisymmetric flow
Edition Identifiers:
- The Open Library ID: OL19379743M
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 Jets and flames in co-flowing streams at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks
By Neil T. Van Dresar
“Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks” Metadata:
- Title: ➤ Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks
- Author: Neil T. Van Dresar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Expulsion - Fluid flow - Fuel tank pressurization - Gas injection - Gas pressure - Liquid hydrogen - Mass flow - Prediction analysis techniques - Statistical analysis
Edition Identifiers:
- The Open Library ID: OL15414433M
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 Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies
By Irina G. Brykina
“An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies” Metadata:
- Title: ➤ An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies
- Author: Irina G. Brykina
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lyndon B. Johnson Space Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Houston, Tex
“An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Blunt bodies - Axisymmetric bodies - Aerodynamic heating - Flow measurement - Hypersonics - Parabolic bodies
Edition Identifiers:
- The Open Library ID: OL15539983M
- Online Computer Library Center (OCLC) ID: 40771789
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 An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Navier–Stokes equations
for creeping flow results when the left side is assumed zero. In axisymmetric flow another stream function formulation, called the Stokes stream function
Stokes' law
flow direction, while r is the radius as measured perpendicular to the z–axis. The origin is at the sphere centre. Because the flow is axisymmetric around
Beltrami flow
immediate consequence of Beltrami flow is that it can never be a planar or axisymmetric flow because in those flows, vorticity is always perpendicular
Taylor–Couette flow
and a secondary steady state characterized by axisymmetric toroidal vortices, known as Taylor vortex flow, emerges. Subsequently, upon increasing the angular
Fredholm integral equation
PMID 10060625. Daddi-Moussa-Ider, A.; Kaoui, B.; Löwen, H. (9 April 2019). "Axisymmetric flow due to a Stokeslet near a finite-sized elastic membrane". Journal
Taylor–Culick flow
In fluid dynamics, Taylor–Culick flow, a type of a stagnation point flow, describes the axisymmetric flow inside a long slender cylinder with one end closed
Hagen–Poiseuille equation
The flow is steady ( ∂.../∂t = 0 ). The radial and azimuthal components of the fluid velocity are zero ( ur = uθ = 0 ). The flow is axisymmetric ( ∂
Stagnation point flow
equipment. The axisymmetric stagnation point flow corresponds to α = β ( λ = 0 ) {\displaystyle \alpha =\beta \,(\lambda =0)} . The flow field can be simply
Waverider
Axisymmetric Flow Fields". Ingenieur-Archiv, 37, Band, 1, Heft, pp. 56-72, 1968. Pike, J. (1–3 May 1968). Experimental Results from Three Cone-Flow Waveriders
Centrifugal compressor
sub-class of dynamic, axisymmetric, work-absorbing turbomachinery. They achieve pressure rise by adding energy to the continuous flow of fluid through the