Explore: Subsonic Flow
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Source: The Open Library
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Search results from The Open Library
1The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
By Norbert Ulbrich
“The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel” Metadata:
- Title: ➤ The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel
- Author: Norbert Ulbrich
- Language: English
- Number of Pages: Median: 186
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor - Available from the National Technical Information Service
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Springfield, VA - Moffett Field, Calif
“The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel” Subjects and Themes:
- Subjects: ➤ Force distribution - Interference (Aerodynamics) - Subsonic flow - Subsonic wind tunnels - Support systems - Wall flow - Wall pressure - Wind tunnel walls
Edition Identifiers:
- The Open Library ID: OL15541289M - OL17597333M - OL20505618M - OL18132454M - OL17131369M
- Online Computer Library Center (OCLC) ID: 41446610
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
By Wendy B. Lessard
“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Metadata:
- Title: ➤ Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
- Author: Wendy B. Lessard
- Language: English
- Number of Pages: Median: 77
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Hampton, Va - Springfield, VA - [Springfield, Va
“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aircraft models - Pressure distribution - Subsonic flow - Unstructured grids (Mathematics) - Angle of attack - Grid generation (Mathematics) - Flow distribution - Aerodynamics - F-16 (Jet fighter plane) - Wind tunnel models - Mathematics - Numerical grid generation (Numerical analysis)
Edition Identifiers:
- The Open Library ID: OL18121254M - OL17581026M - OL19045641M - OL15504440M - OL17126971M
- Online Computer Library Center (OCLC) ID: 40389824
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Implementation of a two-equation K-[omega] turbulence model in NPARC
By Dennis A. Yoder
“Implementation of a two-equation K-[omega] turbulence model in NPARC” Metadata:
- Title: ➤ Implementation of a two-equation K-[omega] turbulence model in NPARC
- Author: Dennis A. Yoder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Implementation of a two-equation K-[omega] turbulence model in NPARC” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent boundary layer - Separated flow - Incompressible flow - Turbulence models - Subsonic flow - Boundary layer flow - Applications programs (Computers) - Transition flow - Transistion flow
Edition Identifiers:
- The Open Library ID: OL15423264M - OL18086918M - OL17117628M - OL17117429M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Higher-order approximations in interactive airfoil calculations
By D. W. Zingg
“Higher-order approximations in interactive airfoil calculations” Metadata:
- Title: ➤ Higher-order approximations in interactive airfoil calculations
- Author: D. W. Zingg
- Language: English
- Number of Pages: Median: 102
- Publisher: ➤ University of Toronto - Institute for Aerospace Studies
- Publish Date: 1987 - 1988
- Publish Location: [Downsview, Ont.]
“Higher-order approximations in interactive airfoil calculations” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layers - Computational fluid dynamics - Incompressible flow - Interactive methods - Pressure gradients - Subsonic flow
Edition Identifiers:
- The Open Library ID: OL20898250M - OL19987220M - OL20697434M
Author's Alternative Names:
"David W. Zingg"Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Analysis of boundary conditions for SSME subsonic internal viscous flow analysis
By Baker, A. J.
“Analysis of boundary conditions for SSME subsonic internal viscous flow analysis” Metadata:
- Title: ➤ Analysis of boundary conditions for SSME subsonic internal viscous flow analysis
- Author: Baker, A. J.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Computational Mechanics Corporation
- Publish Date: 1986
- Publish Location: ➤ Knoxville, TN - [Washington, DC - Springfield, Va
“Analysis of boundary conditions for SSME subsonic internal viscous flow analysis” Subjects and Themes:
- Subjects: ➤ Boundary conditions - Boundary value problems - Finite difference theory - Finite element method - Space shuttle main engine - Subsonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL14985639M - OL17684399M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6STARS
By Kajal K. Gupta
“STARS” Metadata:
- Title: STARS
- Author: Kajal K. Gupta
- Language: English
- Number of Pages: Median: 160
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
- Publish Date: 1990 - 1991
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“STARS” Subjects and Themes:
- Subjects: ➤ Aerodynamic forces - Aeroelasticity - Aeroservoelasticity - Computer programs - Control stability - Finite element method - Structural analysis - Structural analysis (Engineering) - Subsonic flow - Supersonic flow - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL16131038M - OL16132316M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7An extended Lagrangian method
By Meng-Sing Liou
“An extended Lagrangian method” Metadata:
- Title: An extended Lagrangian method
- Author: Meng-Sing Liou
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - [Washington, DC
“An extended Lagrangian method” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Computational grids - Supersonic flow - Subsonic flow - Lagrange equations - Lagrangian function
Edition Identifiers:
- The Open Library ID: OL14698842M - OL15498355M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
By Bernard Spencer
“A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Metadata:
- Title: ➤ A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
- Author: Bernard Spencer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Subjects and Themes:
- Subjects: ➤ Launch vehicles - Lift drag ratio - Wind tunnel tests - Subsonic flow - Assured crew return vehicle - Angle of attack - Pitching moments - Lift - Aerodynamic drag - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL17106590M - OL17685249M
- Online Computer Library Center (OCLC) ID: 35281561
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Description of panel method code ANTARES
By Norbert Ulbrich
“Description of panel method code ANTARES” Metadata:
- Title: ➤ Description of panel method code ANTARES
- Author: Norbert Ulbrich
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2000
- Publish Location: ➤ Moffett, Field, Calif - Hanover, MD
“Description of panel method code ANTARES” Subjects and Themes:
- Subjects: ➤ Aerodynamic interference - Computer programs - Lift - Rectangular wind tunnels - Subsonic flow - Wall flow - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16030491M - OL17607419M
- Online Computer Library Center (OCLC) ID: 50075150
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10An extended Lagrangian method
By M. S. Liou
“An extended Lagrangian method” Metadata:
- Title: An extended Lagrangian method
- Author: M. S. Liou
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1992 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - [Washington, DC
“An extended Lagrangian method” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Computational grids - Supersonic flow - Subsonic flow - Lagrange equations - Lagrangian function
Edition Identifiers:
- The Open Library ID: OL17124619M - OL15383946M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
By S. Paul Pao
“Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Metadata:
- Title: ➤ Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
- Author: S. Paul Pao
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Jet flow - K-epsilon turbulence model - Mach number - Navier-Stokes equation - Subsonic flow - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL17838891M - OL15504438M
- Online Computer Library Center (OCLC) ID: 40386685
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Wing pressure distributions from subsonic tests of a high-wing transport model
By Zachary T. Applin
“Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:
- Title: ➤ Wing pressure distributions from subsonic tests of a high-wing transport model
- Author: Zachary T. Applin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Wing pressure distributions from subsonic tests of a high-wing transport model” Subjects and Themes:
- Subjects: ➤ Angle of attack - Leading edge flaps - Mach number - Pressure distribution - Reynolds number - Sideslip - Subsonic flow - Trailing edge flaps - Transport aircraft - Wind tunnel tests - Wings
Edition Identifiers:
- The Open Library ID: OL17788775M - OL15411003M
- Online Computer Library Center (OCLC) ID: 32865600
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Doppler global velocimetry at NASA Glenn Research Center
By Christian T. Lant
“Doppler global velocimetry at NASA Glenn Research Center” Metadata:
- Title: ➤ Doppler global velocimetry at NASA Glenn Research Center
- Author: Christian T. Lant
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, VA - Hanover, MD
“Doppler global velocimetry at NASA Glenn Research Center” Subjects and Themes:
- Subjects: ➤ Coupling - Doppler effect - Free jets - Pulsed lasers - Subsonic flow - Supersonic flow - Velocity measurement
Edition Identifiers:
- The Open Library ID: OL17633151M - OL17722593M
- Online Computer Library Center (OCLC) ID: 56822084
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14High frequency flow/structural interaction in dense subsonic fluids
By Baw-Lin Liu
“High frequency flow/structural interaction in dense subsonic fluids” Metadata:
- Title: ➤ High frequency flow/structural interaction in dense subsonic fluids
- Author: Baw-Lin Liu
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - National Aeronautics and Space Administration, Marshall Space Flight Center - Rockwell Aerospace, Space Systems Division, Huntsville Operations
- Publish Date: 1994 - 1995
- Publish Location: ➤ Marshall Space Flight Center, Ala - [Springfield, Va - Springfield, Va - [Huntsville, Ala.] - [Washington, DC
“High frequency flow/structural interaction in dense subsonic fluids” Subjects and Themes:
- Subjects: ➤ Aircraft fuel systems - Computational fluid dynamics - Computer aided design - Computer assisted instruction - Critical flow - Data bases - Databases - Dynamic characteristics - Dynamic structural analysis - Fatigue (Materials) - Feed systems - Flow distribution - Fluid-solid interactions - High temperature gases - Internal flow - Load carrying capacity - Structural design criteria - Structural reliability - Subsonic flow - Unsteady flow - Vortex shedding
- Places: United States
Edition Identifiers:
- The Open Library ID: OL15403882M - OL15409454M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Large 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
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16Analytical studies of boundary layer generated aircraft interior noise
By M. S. Howe
“Analytical studies of boundary layer generated aircraft interior noise” Metadata:
- Title: ➤ Analytical studies of boundary layer generated aircraft interior noise
- Author: M. S. Howe
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Boston University, College of Engineering
- Publish Date: 1997
- Publish Location: ➤ Boston, MA - [Washington, DC - Springfield, Va
“Analytical studies of boundary layer generated aircraft interior noise” Subjects and Themes:
- Subjects: ➤ Fuselages - Turbulent flow - Turbulent boundary layer - Boundary layers - Sound waves - Vibration - Wall pressure - Subsonic flow - Aircraft noise - Pressure oscillations
Edition Identifiers:
- The Open Library ID: OL17826943M - OL15491947M
- Online Computer Library Center (OCLC) ID: 39187378
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Advanced method for computing the flow around wings with rear separation and ground effect
By Klaus Jacob
“Advanced method for computing the flow around wings with rear separation and ground effect” Metadata:
- Title: ➤ Advanced method for computing the flow around wings with rear separation and ground effect
- Author: Klaus Jacob
- Number of Pages: Median: 62
- Publisher: ➤ DFVLR Institut fur Theoretische Stromungsmechanik
- Publish Date: 1986
- Publish Location: Gottingen
“Advanced method for computing the flow around wings with rear separation and ground effect” Subjects and Themes:
- Subjects: Ground effect (Aerodynamics) - Subsonic flow - Separated flow - Wings
Edition Identifiers:
- The Open Library ID: OL19987038M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18External boundary conditions for three-dimensional problems of computational aerodynamics
By Semyon V. Tsynkov
“External boundary conditions for three-dimensional problems of computational aerodynamics” Metadata:
- Title: ➤ External boundary conditions for three-dimensional problems of computational aerodynamics
- Author: Semyon V. Tsynkov
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“External boundary conditions for three-dimensional problems of computational aerodynamics” Subjects and Themes:
- Subjects: ➤ Boundary conditions - Computational fluid dynamics - Finite difference theory - Navier-Stokes equation - Subsonic flow - Three dimensional flow - Transonic flow - Viscous fluids
Edition Identifiers:
- The Open Library ID: OL15482790M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Prediction of vortex shedding from circular and noncircular bodies in subsonic flow
By Michael R. Mendenhall
“Prediction of vortex shedding from circular and noncircular bodies in subsonic flow” Metadata:
- Title: ➤ Prediction of vortex shedding from circular and noncircular bodies in subsonic flow
- Author: Michael R. Mendenhall
- Number of Pages: Median: 163
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Prediction of vortex shedding from circular and noncircular bodies in subsonic flow” Subjects and Themes:
- Subjects: Subsonic flow - Vortex shedding
Edition Identifiers:
- The Open Library ID: OL18998280M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Shear flow control of cold and heated rectangular jets by mechanical tabs
By W. H. Brown
“Shear flow control of cold and heated rectangular jets by mechanical tabs” Metadata:
- Title: ➤ Shear flow control of cold and heated rectangular jets by mechanical tabs
- Author: W. H. Brown
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Shear flow control of cold and heated rectangular jets by mechanical tabs” Subjects and Themes:
- Subjects: ➤ Boundary layer flow - Flow measurement - Free jets - Jet flow - Jet mixing flow - Nozzle design - Nozzle flow - Nozzle inserts - Shear flow - Subsonic flow - Supersonic flow - Tabs (Control surfaces)
Edition Identifiers:
- The Open Library ID: OL17002529M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Correction for wall-interference by means of a measured-boundary-conditon method
By Th. E. Labrujere
“Correction for wall-interference by means of a measured-boundary-conditon method” Metadata:
- Title: ➤ Correction for wall-interference by means of a measured-boundary-conditon method
- Author: Th. E. Labrujere
- Number of Pages: Median: 41
- Publisher: National Aerospace Laboratory
- Publish Date: 1984
- Publish Location: Amsterdam
“Correction for wall-interference by means of a measured-boundary-conditon method” Subjects and Themes:
- Subjects: ➤ Subsonic flow - Green's functions - Two dimensional flow - Wind tunnel walls - Three dimensional flow - Potential flow
Edition Identifiers:
- The Open Library ID: OL20982753M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
By Michael K. Ponton
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Metadata:
- Title: ➤ Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
- Author: Michael K. Ponton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Aeroacoustics - Exhaust nozzles - Jet flow - Flow characteristics - Subsonic flow - Convergent nozzles - High Reynolds number - Engine noise - Pressure oscillations
Edition Identifiers:
- The Open Library ID: OL15550628M
Author's Alternative Names:
"Nichael K. Ponton"Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Investigation of parabolic computational techniques for internal high-speed viscous flows
By O. L. Anderson
“Investigation of parabolic computational techniques for internal high-speed viscous flows” Metadata:
- Title: ➤ Investigation of parabolic computational techniques for internal high-speed viscous flows
- Author: O. L. Anderson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - United Technologies Research Center
- Publish Date: 1985
- Publish Location: ➤ East Hartford, CT - Hampton, Va
“Investigation of parabolic computational techniques for internal high-speed viscous flows” Subjects and Themes:
- Subjects: ➤ Supersonic combustion ramjet eingines - Scramjet engines - Mathematical models - Supersonic flow - Subsonic flow - Airplanes
Edition Identifiers:
- The Open Library ID: OL16154860M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Application of chimera grid scheme to combustor flowfields at all speeds
By Shaye Yungster
“Application of chimera grid scheme to combustor flowfields at all speeds” Metadata:
- Title: ➤ Application of chimera grid scheme to combustor flowfields at all speeds
- Author: Shaye Yungster
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Application of chimera grid scheme to combustor flowfields at all speeds” Subjects and Themes:
- Subjects: ➤ Reacting flow - Flow equations - Combustion - Unsteady flow - Combustion chambers - Grid generation (Mathematics) - Subsonic flow
Edition Identifiers:
- The Open Library ID: OL15506510M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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25Response of high subsonic jet to nonaxisymmetric disturbances
By Alvin Bayliss
“Response of high subsonic jet to nonaxisymmetric disturbances” Metadata:
- Title: ➤ Response of high subsonic jet to nonaxisymmetric disturbances
- Author: Alvin Bayliss
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - Reston, VA - [Washington, DC
“Response of high subsonic jet to nonaxisymmetric disturbances” Subjects and Themes:
- Subjects: ➤ Transonic speed - Antenna radiation patterns - Cylindrical coordinates - Subsonic flow - Gas jets - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15509220M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators
By Soo-Yong Cho
“Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators” Metadata:
- Title: ➤ Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators
- Author: Soo-Yong Cho
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Inlet flow - Subsonic flow - Viscous flow - Vortices - Duct geometry - Three dimensional flow - Finite volume method - Navier-Stokes equation - Engine inlets - Compressible flow - Vortex generators
Edition Identifiers:
- The Open Library ID: OL15408550M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27A numerical simulator for three-dimensional flows through vibrating blade rows
By H. Andrew Chuang
“A numerical simulator for three-dimensional flows through vibrating blade rows” Metadata:
- Title: ➤ A numerical simulator for three-dimensional flows through vibrating blade rows
- Author: H. Andrew Chuang
- 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]
“A numerical simulator for three-dimensional flows through vibrating blade rows” Subjects and Themes:
- Subjects: ➤ Subsonic flow - Aeroacoustics - Annular ducts - Three dimensional flow - Turbomachinery - Transonic flow - Rotors - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL15541272M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
By Roger A. Lepsch
“Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Metadata:
- Title: ➤ Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
- Author: Roger A. Lepsch
- 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
“Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle” Subjects and Themes:
- Subjects: ➤ Rolling moments - Fins - Lift drag ratio - Wind tunnel tests - Subsonic flow - Angle of attack - Delta wings - Flow visualization - Wind tunnel models - Satellite control - Directional control
Edition Identifiers:
- The Open Library ID: OL15504620M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29Role of boundary conditions in Monte Carlo simulation of MEMS devices
By Robert P. Nance
“Role of boundary conditions in Monte Carlo simulation of MEMS devices” Metadata:
- Title: ➤ Role of boundary conditions in Monte Carlo simulation of MEMS devices
- Author: Robert P. Nance
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Role of boundary conditions in Monte Carlo simulation of MEMS devices” Subjects and Themes:
- Subjects: Microchannels - Monte Carlo method - Subsonic flow - Boundary conditions
Edition Identifiers:
- The Open Library ID: OL15487321M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
By Elizabeth B. Plentovich
“Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Metadata:
- Title: ➤ Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Author: Elizabeth B. Plentovich
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamic load - Aerodynamics, Transonic - Cavities - Cavities (Airplanes) - Flow distribution - High Reynolds number - Mach number - Pressure distribution - Reynolds number - Subsonic flow - Transonic Aerodynamics - Transonic flow - Turbulent boundary layer - Yaw - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16135213M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31Computational investigations of noise suppression in subsonic round jets
By C. David Pruett
“Computational investigations of noise suppression in subsonic round jets” Metadata:
- Title: ➤ Computational investigations of noise suppression in subsonic round jets
- Author: C. David Pruett
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Computational investigations of noise suppression in subsonic round jets” Subjects and Themes:
- Subjects: Subsonic flow - Computational grids - Noise reduction - Computer programs
Edition Identifiers:
- The Open Library ID: OL15539174M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32RNS applications for interacting sub- and supersonic flows
By Stanley G. Rubin
“RNS applications for interacting sub- and supersonic flows” Metadata:
- Title: ➤ RNS applications for interacting sub- and supersonic flows
- Author: Stanley G. Rubin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“RNS applications for interacting sub- and supersonic flows” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Multigrid methods - Flow distribution - Computational grids - Supersonic flow - Subsonic flow - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15505733M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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33Entry dispersion analysis for the Stardust comet sample return capsule
By Prasun N. Desai
“Entry dispersion analysis for the Stardust comet sample return capsule” Metadata:
- Title: ➤ Entry dispersion analysis for the Stardust comet sample return capsule
- Author: Prasun N. Desai
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Reston, VA - Springfield, Va - [Washington, D.C
“Entry dispersion analysis for the Stardust comet sample return capsule” Subjects and Themes:
- Subjects: ➤ Comets - Descent - High altitude - Atmospheric entry - Subsonic flow - Earth-moon system - Attitude (Inclination) - Angle of attack - Downrange - Monte Carlo method
Edition Identifiers:
- The Open Library ID: OL15498487M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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34Measurement of gust response on a turbine cascade
By Anatole P Kurkov
“Measurement of gust response on a turbine cascade” Metadata:
- Title: ➤ Measurement of gust response on a turbine cascade
- Author: Anatole P Kurkov
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Measurement of gust response on a turbine cascade” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Rotor aerodynamics - Pressure distribution - Annular flow - Rotor blades (Turbomachinery) - Subsonic flow - Gusts - Cascade flow - Turbine blades - Mach number
Edition Identifiers:
- The Open Library ID: OL15411522M
Author's Alternative Names:
"Anatole P. Kurkov"Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Natural rolling responses of a delta wing in transonic and subsonic flows
By Margaret A. Menzies
“Natural rolling responses of a delta wing in transonic and subsonic flows” Metadata:
- Title: ➤ Natural rolling responses of a delta wing in transonic and subsonic flows
- Author: Margaret A. Menzies
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Aeronautics
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Reston, Va - [Springfield, Va
“Natural rolling responses of a delta wing in transonic and subsonic flows” Subjects and Themes:
- Subjects: ➤ Flow equations - Fluid dynamics - Rigid structures - Subsonic flow - Swept wings - Navier-Stokes equation - Slender wings - Delta wings - Transonic flow
Edition Identifiers:
- The Open Library ID: OL15508546M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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36Feasibility study of a single component scanning laser doppler anemometer
By Peter Pulinec
“Feasibility study of a single component scanning laser doppler anemometer” Metadata:
- Title: ➤ Feasibility study of a single component scanning laser doppler anemometer
- Author: Peter Pulinec
- Number of Pages: Median: 46
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1978
- Publish Location: [Downsview, Ont.]
“Feasibility study of a single component scanning laser doppler anemometer” Subjects and Themes:
- Subjects: Laser anemometers - Subsonic flow
Edition Identifiers:
- The Open Library ID: OL19988324M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Pressure distribution and reattachment length of subsonic flow over a rearward-facing step
By Christopher G. Barringer
“Pressure distribution and reattachment length of subsonic flow over a rearward-facing step” Metadata:
- Title: ➤ Pressure distribution and reattachment length of subsonic flow over a rearward-facing step
- Author: Christopher G. Barringer
- Number of Pages: Median: 69
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1979
- Publish Location: [Downsview, Ont.]
“Pressure distribution and reattachment length of subsonic flow over a rearward-facing step” Subjects and Themes:
- Subjects: Subsonic flow
Edition Identifiers:
- The Open Library ID: OL19988486M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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38Application of linearized transonic theory to tunnel blockage interference
By C. F. Lo
“Application of linearized transonic theory to tunnel blockage interference” Metadata:
- Title: ➤ Application of linearized transonic theory to tunnel blockage interference
- Author: C. F. Lo
- Number of Pages: Median: 28
- Publisher: ➤ Arnold Engineering Development Center
- Publish Date: 1974
- Publish Location: Arnold AF Station, Tenn
“Application of linearized transonic theory to tunnel blockage interference” Subjects and Themes:
- Subjects: Transonic flow - Transonic wind tunnels - Subsonic flow - Interference
Edition Identifiers:
- The Open Library ID: OL20983846M
Access and General Info:
- First Year Published: 1974
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Implementation of and measurement with the LIPA technique in a subsonic jet
By R. E. Falco
“Implementation of and measurement with the LIPA technique in a subsonic jet” Metadata:
- Title: ➤ Implementation of and measurement with the LIPA technique in a subsonic jet
- Author: R. E. Falco
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Michigan State University, Dept. of Mechanical Engineering
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC - East Lansing, MI
“Implementation of and measurement with the LIPA technique in a subsonic jet” Subjects and Themes:
- Subjects: ➤ Laser applications - Stress distribution - Photochemical reactions - Vorticity - Phosphorescence - Laser beams - Subsonic flow - Gas jets - Reynolds stress - Velocity measurement - Flow visualization - Turbulence - Stress intensity factors
Edition Identifiers:
- The Open Library ID: OL15404028M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Determination of the pressure drag of airfoils by integration of surface pressures
By William H. Phillips
“Determination of the pressure drag of airfoils by integration of surface pressures” Metadata:
- Title: ➤ Determination of the pressure drag of airfoils by integration of surface pressures
- Author: William H. Phillips
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Determination of the pressure drag of airfoils by integration of surface pressures” Subjects and Themes:
- Subjects: Pressure drag - Airfoil profiles - Subsonic flow - Boundary layer flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15405853M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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41A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
By Richard J. Re
“A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” Metadata:
- Title: ➤ A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- Author: Richard J. Re
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” Subjects and Themes:
- Subjects: ➤ Static pressure - Pressure distribution - Wind tunnel tests - Subsonic flow - Angle of attack - Engine inlets - Aircraft engines - Mach number
Edition Identifiers:
- The Open Library ID: OL15498125M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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42Methods of linearization in compressible flow
By F. Edward Ehlers
“Methods of linearization in compressible flow” Metadata:
- Title: ➤ Methods of linearization in compressible flow
- Author: F. Edward Ehlers
- Number of Pages: Median: 141
- Publisher: ➤ Wright-Patterson Air Force Base
- Publish Date: 1949
- Publish Location: Dayton, Ohio
“Methods of linearization in compressible flow” Subjects and Themes:
- Subjects: Prandtl-Glauert method - Subsonic flow - Compressible flow
Edition Identifiers:
- The Open Library ID: OL19253441M
Access and General Info:
- First Year Published: 1949
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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43Validation of WIND for a series of inlet flows
By John W. Slater
“Validation of WIND for a series of inlet flows” Metadata:
- Title: ➤ Validation of WIND for a series of inlet flows
- Author: John W. Slater
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2002
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Validation of WIND for a series of inlet flows” Subjects and Themes:
- Subjects: Computational fluid dynamics - Hypersonic flow - Inlet flow - Subsonic flow - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL16106756M
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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44Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes
By K. K. Ahuja
“Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes” Metadata:
- Title: ➤ Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes
- Author: K. K. Ahuja
- 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
“Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aerocoustic codes” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Temperature effects - Aeroacoustics - Cavities - Wall jets - Wind tunnel tests - Subsonic flow - Aerodynamic noise - Cavity flow
Edition Identifiers:
- The Open Library ID: OL15415718M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45Unsteady aerodynamics
By A. V. Balakrishman
“Unsteady aerodynamics” Metadata:
- Title: Unsteady aerodynamics
- Author: A. V. Balakrishman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Unsteady aerodynamics” Subjects and Themes:
- Subjects: Inviscid flow - Subsonic flow - Unsteady aerodynamics - Compressible flow
Edition Identifiers:
- The Open Library ID: OL15556993M
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:
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46Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies
By James L. Blackshire
“Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies” Metadata:
- Title: ➤ Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies
- Author: James L. Blackshire
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies” Subjects and Themes:
- Subjects: ➤ Velocity measurement - Particle image velocimetry - Turbulence - Subsonic flow - Gas jets - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15498720M
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:
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47Application of the pressure sensitive paint technique to steady and unsteady flow
By Y. Shimbo
“Application of the pressure sensitive paint technique to steady and unsteady flow” Metadata:
- Title: ➤ Application of the pressure sensitive paint technique to steady and unsteady flow
- Author: Y. Shimbo
- Language: English
- Publisher: ➤ Joint Institute for Aeronautics and Acoustics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - [Stanford, Calif.?] - Springfield, Va
“Application of the pressure sensitive paint technique to steady and unsteady flow” Subjects and Themes:
- Subjects: ➤ Flow measurement - Pressure distribution - Paints - Subsonic flow - Jet impingement - Pressure measurement - Unsteady flow - Steady flow
Edition Identifiers:
- The Open Library ID: OL15499036M
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.
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48Spurious frequencies as a result of numerical boundary treatments
By Saul S. Abarbanel
“Spurious frequencies as a result of numerical boundary treatments” Metadata:
- Title: ➤ Spurious frequencies as a result of numerical boundary treatments
- Author: Saul S. Abarbanel
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Spurious frequencies as a result of numerical boundary treatments” Subjects and Themes:
- Subjects: ➤ Vortex shedding - Perturbation - Boundary value problems - Boundary conditions - Numerical stability - Subsonic flow - Finite difference theory
Edition Identifiers:
- The Open Library ID: OL15411882M
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.
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49USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
By Michael R. Wiese
“USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” Metadata:
- Title: ➤ USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
- Author: Michael R. Wiese
- Language: English
- Number of Pages: Median: 97
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, D.C.]
“USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics” Subjects and Themes:
- Subjects: ➤ Panel method (Fluid dynamics) - Pressure distribution - Aerodynamics - Supersonic flow - Subsonic flow - Aerodynamic characteristics - Computer programs - Potential flow
Edition Identifiers:
- The Open Library ID: OL16122026M
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.
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50Axis switching and spreading of an asymmetric jet
By K. B. M. O. Zaman
“Axis switching and spreading of an asymmetric jet” Metadata:
- Title: ➤ Axis switching and spreading of an asymmetric jet
- Author: K. B. M. O. Zaman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Axis switching and spreading of an asymmetric jet” Subjects and Themes:
- Subjects: ➤ Vortex - Free jets - Jet mixing flow - Tabs (Control surfaces) - Subsonic flow - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15408493M
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:
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