Explore: Aerodynamic Characteristics
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Source: The Open Library
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1A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows
By Matthew D. Montgomery
“A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows” Metadata:
- Title: ➤ A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows
- Author: Matthew D. Montgomery
- Language: English
- Number of Pages: Median: 83
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor] - National Technical Information Service, distributor - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1996 - 1997
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - [Washington, DC]
“A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Mathematical models - Three dimensional models - Unsteady aerodynamics - Three dimensional flow - Aerodynamic characteristics - Boundary conditions - Euler equations of motion - Turbomachine blades - Unsteady flow (Aerodynamics) - Fluid dynamics - Boundary layer - Turbomachines
Edition Identifiers:
- The Open Library ID: ➤ OL18121541M - OL17576345M - OL18121455M - OL18998858M - OL15504972M - OL17576348M - OL17126336M - OL17126578M
- Online Computer Library Center (OCLC) ID: 40238889 - 40154543
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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2First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop
By NASA/Industry High-Speed Research Configuration Aerodynamics Workshop (1st 1996 Hampton, Va.)
“First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop” Metadata:
- Title: ➤ First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop
- Author: ➤ NASA/Industry High-Speed Research Configuration Aerodynamics Workshop (1st 1996 Hampton, Va.)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, [distributor
- Publish Date: 1999
- Publish Location: Springfield, VA - Hampton, Va
“First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Civil aviation - Computational fluid dynamics - Congresses - Control stability - Government/industry relations - Government/industry relations.. - High-speed aeronautics - Supersonic transports - Aerodynamics
Edition Identifiers:
- The Open Library ID: ➤ OL18141427M - OL17596208M - OL18318831M - OL15576729M - OL22406716M - OL18302383M - OL14513189M
- Online Computer Library Center (OCLC) ID: 45110415
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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31999 NASA High-Speed Research Program Aerodynamic Performance Workshop
By NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)
“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Metadata:
- Title: ➤ 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
- Author: ➤ NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aerodynamic stability - Aerodynamics - Aerodynamics, Supersonic - Aeronautics, Commercial - Aircraft design - Airplanes - Body-wing configurations - Canard configurations - Civil aviation - Commercial Aeronautics - Computational fluid dynamics - Congresses - Design and construction - Engine airframe integration - High-speed aeronautics - Optimization - Performance prediction - Research - Supersonic Aerodynamics - Supersonic transports - Wind tunnel tests - Wing nacelle configurations
Edition Identifiers:
- The Open Library ID: OL18140721M - OL18296463M - OL22405471M - OL15573231M - OL17594870M
- Online Computer Library Center (OCLC) ID: 44596209
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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4Missile aerodynamics
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Missile aerodynamics” Metadata:
- Title: Missile aerodynamics
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 388
- Publisher: Sine nomine - AGARD
- Publish Date: 1978 - 1990
- Publish Location: ➤ Neuilly-sur-Seine - S.l - Neuilly sur Seine, France - Neuilly-sur-Seine, France
“Missile aerodynamics” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Missiles
Edition Identifiers:
- The Open Library ID: OL21334937M - OL21699143M - OL21334660M - OL20117001M
- All ISBNs: 9283505891 - 9789283505891
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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5Assessment of dual-point drag reduction for an executive-jet modified airfoil section
By Dennis O. Allison
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Metadata:
- Title: ➤ Assessment of dual-point drag reduction for an executive-jet modified airfoil section
- Author: Dennis O. Allison
- Language: English
- Number of Pages: Median: 114
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from National Technical Information Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langly Research Center
- Publish Date: 1996
- Publish Location: ➤ Hampton, Virginia - Springfield, VA - Hampton, Va - [Springfield, Va
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Subjects and Themes:
- Subjects: ➤ Drag reduction - Reynolds number - Boundary layer transition - Angle of attack - Pitching moments - Transonic wind tunnels - Airfoil profiles - Force distribution - Trailing edges - Aerodynamic characteristics - Aerodynamics - Aerofoils
Edition Identifiers:
- The Open Library ID: OL19049550M - OL18121248M - OL17126940M - OL17581020M - OL15504416M
- Online Computer Library Center (OCLC) ID: 40386607
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
By David E. Hahne
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Metadata:
- Title: ➤ Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Springfield, VA - Hampton, Va
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic coefficients - Aerodynamic stability - Aerodynamics, Hypersonic - Angle of attack - Hypersonic Aerodynamics - Hypersonic speed - Hypersonic vehicles - Low speed - Mach number - Pitching moments - Stability - Stability of airplanes - Stabilizers (Fluid dynamics) - Vortices - Waveriders - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL18134999M - OL17133262M - OL17839424M - OL21033491M - OL15549003M
- Online Computer Library Center (OCLC) ID: 42055832
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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7Numerical solutions of the complete Navier-Stokes equations
By H. A. Hassan
“Numerical solutions of the complete Navier-Stokes equations” Metadata:
- Title: ➤ Numerical solutions of the complete Navier-Stokes equations
- Author: H. A. Hassan
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, North Carolina State University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989 - 1994 - 1995 - 1996
- Publish Location: ➤ [Washington, DC - [Washington, D.C - Raleigh, N.C - Springfield, Va
“Numerical solutions of the complete Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Navier-Stokes equation - Turbulent flow - Turbulence models - Eddy viscosity - Flow velocity - Supersonic combustion - Mixing layers (Fluids) - Jet flow - Navier-Stokes equations - Compressible flow - Compressibility - Numerical solutions - Turbulent mixing - Computational fluid dynamics - Numerical analysis - Vorticity - Boundary layer separation - Vortices - Pressure gradients - Three dimensional flow - Aerodynamic characteristics - Airfoils
Edition Identifiers:
- The Open Library ID: OL15419184M - OL15452379M - OL16135487M - OL14706079M
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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8Development of the X-33 aerodynamic uncertainty model
By Brent R. Cobleigh
“Development of the X-33 aerodynamic uncertainty model” Metadata:
- Title: ➤ Development of the X-33 aerodynamic uncertainty model
- Author: Brent R. Cobleigh
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ National Technical Information Service, distributor - Dryden Flight Research Center - Distributed by the National Aeronautics and Space Administration] - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ Edwards, Calif - [Washington, D.C - [Springfield, Va
“Development of the X-33 aerodynamic uncertainty model” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamics - Design and construction - Flight control - Hypersonics - Launch vehicles (Astronautics) - Lifting bodies - Mathematical models - Monte Carlo method - Reusable space vehicles - Space shuttle orbiters - X-33 reusable launch vehicle
Edition Identifiers:
- The Open Library ID: OL17135415M - OL19395543M - OL17701288M - OL18134932M - OL17591854M
- Online Computer Library Center (OCLC) ID: 42758571
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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9Low-speed longitudinal and lateral-directional aerodynamic characteristics of the X-31 configuration
By Daniel W. Banks
“Low-speed longitudinal and lateral-directional aerodynamic characteristics of the X-31 configuration” Metadata:
- Title: ➤ Low-speed longitudinal and lateral-directional aerodynamic characteristics of the X-31 configuration
- Author: Daniel W. Banks
- Language: English
- Number of Pages: Median: 336
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Low-speed longitudinal and lateral-directional aerodynamic characteristics of the X-31 configuration” Subjects and Themes:
- Subjects: Aerodynamics - X-31 aircraft - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17107169M - OL18055953M - OL15367749M - OL19246585M - OL16383018M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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101998 NASA High-Speed Research Program Aerodynamic Performance Workshop
By NASA High-Speed Research Program Aerodynamic Performance Workshop (1998 Los Angeles, Calif.)
“1998 NASA High-Speed Research Program Aerodynamic Performance Workshop” Metadata:
- Title: ➤ 1998 NASA High-Speed Research Program Aerodynamic Performance Workshop
- Author: ➤ NASA High-Speed Research Program Aerodynamic Performance Workshop (1998 Los Angeles, Calif.)
- 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
“1998 NASA High-Speed Research Program Aerodynamic Performance Workshop” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aerodynamics - Aerodynamics, Supersonic - Aeronautics, Commercial - Aircraft design - Airplanes - Civil aviation - Commercial Aeronautics - Computational fluid dynamics - Congresses - Design and construction - Engine airframe integration - High speed - High-speed aeronautics - NASA programs - Optimization - Research - Supersonic Aerodynamics - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL18302298M - OL17596712M - OL18141561M - OL22407966M - OL15577769M
- Online Computer Library Center (OCLC) ID: 45080512
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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111997 NASA High-Speed Research Program Aerodynamic Performance Workshop
By NASA High-Speed Research Program Aerodynamic Performance Workshop (1997 Hampton, Va.)
“1997 NASA High-Speed Research Program Aerodynamic Performance Workshop” Metadata:
- Title: ➤ 1997 NASA High-Speed Research Program Aerodynamic Performance Workshop
- Author: ➤ NASA High-Speed Research Program Aerodynamic Performance Workshop (1997 Hampton, Va.)
- 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
“1997 NASA High-Speed Research Program Aerodynamic Performance Workshop” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aerodynamics - Airplanes - Civil aviation - Commercial Aeronautics - Congresses - Design and construction - High speed - High-speed aeronautics - Research - Supersonic Aerodynamics - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL18302318M - OL15577814M - OL22407973M - OL17596209M - OL18141566M
- Online Computer Library Center (OCLC) ID: 45096649
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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12Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
By Long P. Yip
“Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Metadata:
- Title: ➤ Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
- Author: Long P. Yip
- Language: English
- Publisher: ➤ National; Aeronautics and Space Administration Scientific and Technical Information Branch - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: [s.l.] - [Washington, D.C.]
“Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Subjects and Themes:
- Subjects: ➤ Control stability - Canard configurations - Control surfaces - Wind tunnel tests - General aviation aircraft - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL13839737M - OL16116833M - OL18218708M
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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13Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
By W. Pelham Phillips
“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Metadata:
- Title: ➤ Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
- Author: W. Pelham Phillips
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Subjects and Themes:
- Subjects: ➤ Spacecraft configurations - Controllability - Supersonic speed - Subsonic speed - Aerodynamic characteristics - Single stage to orbit vehicles - Longitudinal stability - Hypersonics
Edition Identifiers:
- The Open Library ID: OL17516416M - OL17121322M - OL18100856M - OL17687502M
- Online Computer Library Center (OCLC) ID: 38290177
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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14Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications
By Arthur C. Taylor
“Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications” Metadata:
- Title: ➤ Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications
- Author: Arthur C. Taylor
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Old Dominion University Research Foundation - Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University
- Publish Date: 1992 - 1993 - 1994 - 1996
- Publish Location: ➤ Norfolk, Va - Springfield, Va - [Washington, DC - [Springfield, Va - [Washington, D.C
“Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Airfoils - Algorithms - Architecture (Computers) - Computational fluid dynamics - Design analysis - Iterative solution - Linear equations - Matrices (Mathematics) - Memory (Computers) - Navier-Stokes equation - Optimization - Sensitivity - Software tools - Supersonic flow - Turbulent flows - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15359487M - OL17030214M - OL15402708M - OL15498963M
- Online Computer Library Center (OCLC) ID: 32752276
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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15The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge
By Peter W. Duck
“The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge” Metadata:
- Title: ➤ The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge
- 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: 1997
- Publish Location: [Springfield, Va - Hampton, VA
“The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge” Subjects and Themes:
- Subjects: ➤ Supersonic flow - Free flow - Uniform flow - Aerodynamic stability - Aerodynamic characteristics - Wedges - Fourier series - Shock waves
Edition Identifiers:
- The Open Library ID: OL17564669M - OL15485941M - OL18114303M - OL17123820M
- Online Computer Library Center (OCLC) ID: 39284442
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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16Hi-alpha forebody design
By William H. Mason
“Hi-alpha forebody design” Metadata:
- Title: Hi-alpha forebody design
- Author: William H. Mason
- Language: English
- Publisher: ➤ Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University - National Aeronautics and Space Administration - National Technical Information Service, distributor]
- Publish Date: 1992
- Publish Location: ➤ Springfield, Va - [Washington, DC - Blacksburg, VA
“Hi-alpha forebody design” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Computational fluid dynamics - Aircraft design - Fluid dynamics - Directional stability - Turbulence models - Forebodies - Aerodynamic characteristics - Shapes - Flow distribution
Edition Identifiers:
- The Open Library ID: OL18056618M - OL17677233M - OL16126783M - OL18228737M
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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17Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops
By Zachary T. Applin
“Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops” Metadata:
- Title: ➤ Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops
- Author: Zachary T. Applin
- Language: English
- Number of Pages: Median: 63
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ Springfield, Va - Hampton, Va - [Washington, D.C.]
“Low-speed stability and control characteristics of a transport model with aft-fuselage-mounted advanced turboprops” Subjects and Themes:
- Subjects: ➤ Transport aircraft - Turboprop transports - Aerodynamic stability - Aerodynamic characteristics - Control stability - Stability of airplanes - Turboprop engines - Propellers - Stability
Edition Identifiers:
- The Open Library ID: OL17724273M - OL18468444M - OL18217657M - OL19986439M
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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18Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance
By Nateri K. Madavan
“Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance” Metadata:
- Title: ➤ Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance
- Author: Nateri K. Madavan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance” Subjects and Themes:
- Subjects: Supersonic turbines - Design analysis - Fluid dynamics - Navier-Stokes equation - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17839330M - OL18134349M - OL15546637M - OL17131903M
- Online Computer Library Center (OCLC) ID: 41598306
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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19Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
By Daniel W. Banks
“Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” Metadata:
- Title: ➤ Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
- Author: Daniel W. Banks
- Language: English
- Number of Pages: Median: 112
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” Subjects and Themes:
- Subjects: Trailing edge flaps - Canard configurations - Spanwise blowing - Low speed - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL20986801M - OL18080186M - OL17683879M - OL17115110M
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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20Low-speed wind tunnel tests of two waverider configuration models
By Robert J. Pegg
“Low-speed wind tunnel tests of two waverider configuration models” Metadata:
- Title: ➤ Low-speed wind tunnel tests of two waverider configuration models
- Author: Robert J. Pegg
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Low-speed wind tunnel tests of two waverider configuration models” Subjects and Themes:
- Subjects: ➤ Flight characteristics - Directional stability - Lift drag ratio - Wind tunnel tests - Aircraft configurations - Subsonic speed - Aerodynamic stability - Angle of attack - Pitching moments - Waveriders - Lateral stability - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17565252M - OL18118663M - OL15498353M - OL17124624M
- Online Computer Library Center (OCLC) ID: 39554715
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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21X-38 vehicle 131 flutter assessment
By James P. Smith - undifferentiated
“X-38 vehicle 131 flutter assessment” Metadata:
- Title: ➤ X-38 vehicle 131 flutter assessment
- Author: ➤ James P. Smith - undifferentiated
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ National Aeronautics and Space Administration, Lyndon B. Johnson Space Center - National Aeronautics and Space Administration - National Technical Information Service, distributor - Lyndon B. Johnson Space Center - Available from the Center for AeroSpace Information]
- Publish Date: 1997
- Publish Location: ➤ Washington, D.C - [Springfield, Va - [Houston, Tex.] - [Linthicum Heights, MD
“X-38 vehicle 131 flutter assessment” Subjects and Themes:
- Subjects: ➤ Aerodynamic balance - Aerodynamic characteristics - Aerodynamic forces - Airplanes - Control surfaces - Damping - Fins - Flutter (Aerodynamics) - Flutter analysis - Launch vehicles (Astronautics) - Mathematical models - Reusable space vehicles - Rudders - X-38 crew return vehicle
Edition Identifiers:
- The Open Library ID: OL18502902M - OL17125520M - OL17569015M - OL19158282M
- Online Computer Library Center (OCLC) ID: 39850867
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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22Determining the accuracy of aerodynamic model parameters estimated from flight test data
By Eugene A. Morelli
“Determining the accuracy of aerodynamic model parameters estimated from flight test data” Metadata:
- Title: ➤ Determining the accuracy of aerodynamic model parameters estimated from flight test data
- Author: Eugene A. Morelli
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Determining the accuracy of aerodynamic model parameters estimated from flight test data” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Aerodynamic coefficients - Maximum likelihood estimates - Monte Carlo method - Research vehicles
Edition Identifiers:
- The Open Library ID: OL17122769M - OL17695368M - OL17827039M
- Online Computer Library Center (OCLC) ID: 38860609
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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23Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel
By Charles D. Harris
“Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Metadata:
- Title: ➤ Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel
- Author: Charles D. Harris
- Number of Pages: Median: 137
- Publisher: Langley Research Center
- Publish Date: 1981
- Publish Location: Hampton, Va
“Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Airfoils - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19750282M - OL21333674M
Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
By Arthur E. Phelps
“Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Metadata:
- Title: ➤ Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
- Author: Arthur E. Phelps
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Subjects and Themes:
- Subjects: ➤ Military helicopters - Helicopter performance - Wind tunnel tests - Scale models - Aerodynamic characteristics - Stability - Testing - P-531 helicopter
Edition Identifiers:
- The Open Library ID: OL16115009M - OL18217713M - OL18468562M
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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25Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
By Stacey J. Cotton
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Metadata:
- Title: ➤ Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
- Author: Stacey J. Cotton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Buffeting - Flight tests - Flow visualization - Liquid-vapor interfaces - Scale models - Sideslip - Stabilizers (Fluid dynamics) - Tail assemblies - Vortices - Water tunnel tests - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17001977M - OL17682958M - OL18076527M
- Online Computer Library Center (OCLC) ID: 32298726
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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26Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)
By Jack D. Stephenson
“Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” Metadata:
- Title: ➤ Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)
- Author: Jack D. Stephenson
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA)” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aircraft performance - Handling characteristics - Lateral Stability of airplanes - Lateral control - Lateral stability - Research aircraft - Short haul aircraft - Short take-off and landing aircraft - Stability augmentation - Stability of airplanes, Lateral
Edition Identifiers:
- The Open Library ID: OL17630343M - OL18262996M - OL16137756M
- Online Computer Library Center (OCLC) ID: 25291172
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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27Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations
By Gregory M. Gatlin
“Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations” Metadata:
- Title: ➤ Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations
- Author: Gregory M. Gatlin
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerospace planes - Body-wing configurations - Hypersonic flow - Hypersonic planes - Lift (Aerodynamics) - Lift - Aircraft design
Edition Identifiers:
- The Open Library ID: OL19380187M - OL18263011M - OL16137788M
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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28Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
By Guy T. Kemmerly
“Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” Metadata:
- Title: ➤ Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
- Author: Guy T. Kemmerly
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ Langley Research Center - For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - Hampton, Va - [Washington, D.C.]
“Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Short takeoff aircraft - Aircraft landing - Ground effect (Aerodynamics) - Aircraft configurations - Landing - Aerodynamic characteristics - Ground effect - Ground tests
Edition Identifiers:
- The Open Library ID: OL18257141M - OL20268762M - OL16135235M
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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29Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
By Gregory M. Catlin
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Metadata:
- Title: ➤ Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
- Author: Gregory M. Catlin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Flow visualization - Forebodies - Highly maneuverable aircraft - Lift - Low aspect ratio wings - Low speed - Pitching moments - Swept wings - Wind tunnel tests - Wing planforms
Edition Identifiers:
- The Open Library ID: OL17041056M - OL15426200M - OL18088687M
- Online Computer Library Center (OCLC) ID: 35587781
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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30In-flight aerodynamic measurements of an iced horizontal tailplane
By Thomas P. Ratvasky
“In-flight aerodynamic measurements of an iced horizontal tailplane” Metadata:
- Title: ➤ In-flight aerodynamic measurements of an iced horizontal tailplane
- Author: Thomas P. Ratvasky
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“In-flight aerodynamic measurements of an iced horizontal tailplane” Subjects and Themes:
- Subjects: ➤ Flight characteristics - Aircraft icing - Aerodynamics - Wind tunnel tests - Horizontal tail surfaces - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL18134755M - OL17133128M - OL17583227M
- Online Computer Library Center (OCLC) ID: 42013602
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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31Simulation-based analysis of reentry dynamics for the SHARP atmospheric entry vehicle
By Clemens Emmanuel Tillier
“Simulation-based analysis of reentry dynamics for the SHARP atmospheric entry vehicle” Metadata:
- Title: ➤ Simulation-based analysis of reentry dynamics for the SHARP atmospheric entry vehicle
- Author: Clemens Emmanuel Tillier
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Simulation-based analysis of reentry dynamics for the SHARP atmospheric entry vehicle” Subjects and Themes:
- Subjects: ➤ Lifting bodies - Flight control - Thermal protection - Computerized simulation - Trajectory control - Atmospheric entry - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17597481M - OL15547988M - OL18134709M
- Online Computer Library Center (OCLC) ID: 42654720
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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32Development of multiobjective optimization techniques for sonic boom minimization
By Aditi Chattopadhyay
“Development of multiobjective optimization techniques for sonic boom minimization” Metadata:
- Title: ➤ Development of multiobjective optimization techniques for sonic boom minimization
- Author: Aditi Chattopadhyay
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: ➤ Springfield, Va - [Washington, D.C - [Washington, DC
“Development of multiobjective optimization techniques for sonic boom minimization” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Body-wing configurations - Finite element method - Multidisciplinary design optimization - Navier-Stokes equation - Noise reduction - Panel method (Fluid dynamics) - Sonic booms
Edition Identifiers:
- The Open Library ID: OL15540258M - OL17070093M - OL17597201M
- Online Computer Library Center (OCLC) ID: 34770318 - 40708935
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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33Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions
By Farhad Ghaffari
“Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions” Metadata:
- Title: ➤ Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions
- Author: Farhad Ghaffari
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2002
- Publish Location: Hampton, VA - [Springfield, Va
“Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Low aspect ratio wings - Semispan models - Turbulent flow - Wind tunnel tests - Navier-Stokes equation - Lift - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17725170M - OL18227514M - OL19146725M
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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34Launch vehicle flight dynamics
By John E. Cochran
“Launch vehicle flight dynamics” Metadata:
- Title: Launch vehicle flight dynamics
- Author: John E. Cochran
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Launch vehicle flight dynamics” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Aircraft stability - Flight control - Launch vehicles - Payloads
Edition Identifiers:
- The Open Library ID: OL17796471M - OL15423103M
- Online Computer Library Center (OCLC) ID: 35246468
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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35Reducing wind tunnel data requirements using neural networks
By James C. Ross
“Reducing wind tunnel data requirements using neural networks” Metadata:
- Title: ➤ Reducing wind tunnel data requirements using neural networks
- Author: James C. Ross
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Reducing wind tunnel data requirements using neural networks” Subjects and Themes:
- Subjects: ➤ Accuracy - Aerodynamic characteristics - Aerodynamic drag - Data reduction - Neural nets - Pitching moments - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17837960M - OL15542964M
- Online Computer Library Center (OCLC) ID: 40638566
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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36Modeling of aircraft unsteady aerodynamic characteristics
By Vladislav Klein
“Modeling of aircraft unsteady aerodynamic characteristics” Metadata:
- Title: ➤ Modeling of aircraft unsteady aerodynamic characteristics
- Author: Vladislav Klein
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994 - 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Modeling of aircraft unsteady aerodynamic characteristics” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Applications programs (Computers) - F-18 aircraft - Stability derivatives - Stability of airplanes - Unsteady aerodynamics - X-31 aircraft
Edition Identifiers:
- The Open Library ID: OL15398601M - OL15498106M
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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37Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data
By Michael D. Messina
“Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data” Metadata:
- Title: ➤ Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data
- Author: Michael D. Messina
- 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
“Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic coefficients - Flight simulation - Flight tests - Forebodies - Strakes - Yawing moments
Edition Identifiers:
- The Open Library ID: OL15423138M - OL17796495M
- Online Computer Library Center (OCLC) ID: 35248154
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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38Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
By Oktay Baysal
“Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization” Metadata:
- Title: ➤ Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization
- Author: Oktay Baysal
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C - Norfolk, Va
“Domain decomposition for aerodynamic and aeroacoustic analyses, and optimization” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic characteristics - Airfoils - Cavity flow - Computational fluid dynamics - Partial Differential equations - Unstructured grids (Mathematics)
Edition Identifiers:
- The Open Library ID: OL17796518M - OL15423196M
- Online Computer Library Center (OCLC) ID: 35268604
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Aerodynamics of combat aircraft controls and of ground effects
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Aerodynamics of combat aircraft controls and of ground effects” Metadata:
- Title: ➤ Aerodynamics of combat aircraft controls and of ground effects
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 340
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Aerodynamics of combat aircraft controls and of ground effects” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Control surfaces - Fighter aircraft
Edition Identifiers:
- The Open Library ID: OL21333584M - OL20116980M
- All ISBNs: 9789283505556 - 9283505557
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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40Aerodynamics of rotorcraft
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Aerodynamics of rotorcraft” Metadata:
- Title: Aerodynamics of rotorcraft
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 285
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly-sur-Seine - Neuilly sur Seine, France
“Aerodynamics of rotorcraft” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Rotary wing aircraft
Edition Identifiers:
- The Open Library ID: OL21335056M - OL20124791M
- All ISBNs: 9283505921 - 9789283505921
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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41Computation of three-dimensional boundary layers including separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Computation of three-dimensional boundary layers including separation” Metadata:
- Title: ➤ Computation of three-dimensional boundary layers including separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Publisher: Sine nomine - AGARD
- Publish Date: 1987
- Publish Location: ➤ S.l - Neuilly sur Seine, France
“Computation of three-dimensional boundary layers including separation” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Boundary layer flow - Boundary layer separation - Boundary layer transition - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL21697122M - OL18999282M
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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42Calculation of aerodynamic characteristics at high angles of attack for airplane configurations
By C. Edward Lan
“Calculation of aerodynamic characteristics at high angles of attack for airplane configurations” Metadata:
- Title: ➤ Calculation of aerodynamic characteristics at high angles of attack for airplane configurations
- Author: C. Edward Lan
- Language: English
- Publisher: ➤ Flight Research Laboratory, the University of Kansas Center for Research, Inc. - National Technical Information Service, distributor] - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ Lawrence, Kan - Springfield, Va - [Washington, DC
“Calculation of aerodynamic characteristics at high angles of attack for airplane configurations” Subjects and Themes:
- Subjects: Aerodynamic characteristics - F-106 aircraft - F-16 aircraft - F-18 aircraft - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17683865M - OL14980978M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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43Development and implementation of software for visualizing and editing multidimensional flight simulation input data
By Todd Michael Whelan
“Development and implementation of software for visualizing and editing multidimensional flight simulation input data” Metadata:
- Title: ➤ Development and implementation of software for visualizing and editing multidimensional flight simulation input data
- Author: Todd Michael Whelan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Development and implementation of software for visualizing and editing multidimensional flight simulation input data” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Graphical user interface - Aircraft models - Computerized simulation - Windows (Computer programs)
Edition Identifiers:
- The Open Library ID: OL17837370M - OL17697882M
- Online Computer Library Center (OCLC) ID: 40128311
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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44Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
By Lawrence E. Putnam
“Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration” Metadata:
- Title: ➤ Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration
- Author: Lawrence E. Putnam
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Airplanes - Body-wing configurations - Design and construction - Longitudinal Stability of airplanes - Nacelles - Stability of airplanes, Longitudinal - Transonic speed - Transport aircraft - Transport planes - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16116642M - OL18218653M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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45Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
By Bruce Charles
“Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” Metadata:
- Title: ➤ Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
- Author: Bruce Charles
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Airfoils - Noise pollution - Aerodynamic loads - Dynamic characteristics - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17591432M - OL15552422M
- Online Computer Library Center (OCLC) ID: 42623818
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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46Non-linear unsteady wing theory
By J. E. McCune
“Non-linear unsteady wing theory” Metadata:
- Title: ➤ Non-linear unsteady wing theory
- Author: J. E. McCune
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Non-linear unsteady wing theory” Subjects and Themes:
- Subjects: ➤ Aircraft maneuvers - Computational fluid dynamics - Unsteady flow - Control surfaces - Interactional aerodynamics - Wings - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17683867M - OL18080139M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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47Analysis of flowfields over four-engine DC-X rockets
By Ten-See Wang
“Analysis of flowfields over four-engine DC-X rockets” Metadata:
- Title: ➤ Analysis of flowfields over four-engine DC-X rockets
- Author: Ten-See Wang
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC - Reston, VA
“Analysis of flowfields over four-engine DC-X rockets” Subjects and Themes:
- Subjects: ➤ Launch vehicle configurations - Computer programs - Procedures - Conical bodies - Proving - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15541887M - OL17838726M
- Online Computer Library Center (OCLC) ID: 41161388
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:
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48Wing-section optimization for supersonic viscous flows
By Cem C. Item
“Wing-section optimization for supersonic viscous flows” Metadata:
- Title: ➤ Wing-section optimization for supersonic viscous flows
- Author: Cem C. Item
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Wing-section optimization for supersonic viscous flows” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aicraft design - Airfoils - Applications programs (Computers) - Computational fluid dynamics - Inviscid flow - Navier-Stokes equation - Optimization - Supersonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL18084626M - OL17078549M
- Online Computer Library Center (OCLC) ID: 34609263
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:
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49Mechanical design of high lift systems for high aspect ratio swept wings
By Peter K. C. Rudolph
“Mechanical design of high lift systems for high aspect ratio swept wings” Metadata:
- Title: ➤ Mechanical design of high lift systems for high aspect ratio swept wings
- Author: Peter K. C. Rudolph
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Mechanical design of high lift systems for high aspect ratio swept wings” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Boeing 757 aircraft - Design analysis - European Airbus - Lift
Edition Identifiers:
- The Open Library ID: OL15548655M - OL17595589M
- Online Computer Library Center (OCLC) ID: 41969370
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:
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50Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration
By Bryan A. Campbell
“Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration” Metadata:
- Title: ➤ Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration
- Author: Bryan A. Campbell
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Hampton, Va - Springfield, VA - Hanover, MD
“Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Civil aviation - Flow distribution - High speed - Subsonic wind tunnels - Supersonic transports - Vortices
Edition Identifiers:
- The Open Library ID: OL15569348M - OL17595529M
- Online Computer Library Center (OCLC) ID: 44442230
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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Source: Google Books
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1Longitudinal Aerodynamic Characteristics of a Tension Shell Entry Configuration at Mach 20
By Theodore R. Creel
“Longitudinal Aerodynamic Characteristics of a Tension Shell Entry Configuration at Mach 20” Metadata:
- Title: ➤ Longitudinal Aerodynamic Characteristics of a Tension Shell Entry Configuration at Mach 20
- Author: Theodore R. Creel
- Language: English
- Number of Pages: 36
- Genres: Aerodynamic characteristics
Edition Identifiers:
- Google Books ID: SFCdqY0y3f8C
Free Online Preview
- Public Domain: Yes
- Availability Status: Fully available
- Availability Status for country: US.
- Available Formats: Text is not avialbe, image copy is available.
- Google Books Link: Google Books
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2A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies
By Gerald N. Malcolm and Gary T. Chapman
“A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies” Metadata:
- Title: ➤ A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies
- Authors: Gerald N. MalcolmGary T. Chapman
- Language: English
- Number of Pages: 40
- Genres: Aerodynamic characteristics
Edition Identifiers:
- Google Books ID: RFcAxyTgEUUC
Free Online Preview
- Public Domain: Yes
- Availability Status: Fully available
- Availability Status for country: US.
- Available Formats: Text is not avialbe, image copy is available.
- Google Books Link: Google Books
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3Subsonic Longitudinal Aerodynamic Characteristics of a 40 ̊semiapex Angle Conical Reentry Configuration
By W. Pelham Phillips
“Subsonic Longitudinal Aerodynamic Characteristics of a 40 ̊semiapex Angle Conical Reentry Configuration” Metadata:
- Title: ➤ Subsonic Longitudinal Aerodynamic Characteristics of a 40 ̊semiapex Angle Conical Reentry Configuration
- Author: W. Pelham Phillips
- Language: English
- Number of Pages: 20
- Genres: Aerodynamic characteristics
Edition Identifiers:
- Google Books ID: Xy5oVVuxbx8C
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4Effect of Rearward Body Strakes on the Transonic Aerodynamic Characteristics of an Unswept-wing Fighter Aircraft
By C. Robert Carter
“Effect of Rearward Body Strakes on the Transonic Aerodynamic Characteristics of an Unswept-wing Fighter Aircraft” Metadata:
- Title: ➤ Effect of Rearward Body Strakes on the Transonic Aerodynamic Characteristics of an Unswept-wing Fighter Aircraft
- Author: C. Robert Carter
- Language: English
- Number of Pages: 44
- Genres: Aerodynamic characteristics
Edition Identifiers:
- Google Books ID: 87Bm-duxahMC
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