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Source: The Open Library
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1First 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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21999 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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3Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration
By F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.)
“Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration” Metadata:
- Title: ➤ Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration
- Author: ➤ F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.)
- Language: English
- Publisher: ➤ The Division - National Technical Information Service, distributor]
- Publish Date: 1996
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration” Subjects and Themes:
- Subjects: ➤ Congresses - History - Research - Supercritical wings - Airplanes - Fly-by-wire control - Crusader (Jet fighter plane) - Test pilots - F-8 aircraft - Wing profiles - Flight test vehicles - Fly by wire control - Aerodynamic configurations - Aircraft control
- Places: United States
Edition Identifiers:
- The Open Library ID: ➤ OL22393155M - OL558863M - OL18137993M - OL20680769M - OL14503410M - OL15557654M
- Online Computer Library Center (OCLC) ID: 42639244
- Library of Congress Control Number (LCCN): 96142066
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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4Large-scale parallel unstructured mesh computations for 3D high-lift analysis
By Dimitri Mavriplis
“Large-scale parallel unstructured mesh computations for 3D high-lift analysis” Metadata:
- Title: ➤ Large-scale parallel unstructured mesh computations for 3D high-lift analysis
- Author: Dimitri Mavriplis
- Language: English
- Number of Pages: Median: 21
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Springfield, VA - Hampton, VA
“Large-scale parallel unstructured mesh computations for 3D high-lift analysis” Subjects and Themes:
- Subjects: ➤ Parallel computers - Supercomputers - Computational grids - Unstructured grids (Mathematics) - Aerodynamic configurations - Data processing - Aerodynamics - Computational grids (Computer systems) - Numerical grid generation (Numerical analysis)
Edition Identifiers:
- The Open Library ID: OL15548920M - OL17132940M - OL18134971M - OL17583299M - OL19394349M
- Online Computer Library Center (OCLC) ID: 41984851
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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51998 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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61997 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
Online Access
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7Two-dimensional high-lift aerodynamic optimization using neural networks
By Roxana M. Greenman
“Two-dimensional high-lift aerodynamic optimization using neural networks” Metadata:
- Title: ➤ Two-dimensional high-lift aerodynamic optimization using neural networks
- Author: Roxana M. Greenman
- 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
“Two-dimensional high-lift aerodynamic optimization using neural networks” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computers - Navier-Stokes equation - Lift - Neural nets - Airfoils - Aerodynamic configurations - Angle of attack - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL17129961M - OL17580142M - OL18132744M - OL15542052M
- Online Computer Library Center (OCLC) ID: 41151565
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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8Pseudo-time method for optimal shape design using the Euler equations
By Angelo Iollo
“Pseudo-time method for optimal shape design using the Euler equations” Metadata:
- Title: ➤ Pseudo-time method for optimal shape design using the Euler equations
- Author: Angelo Iollo
- Language: English
- Number of Pages: Median: 21
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Hampton, VA - Hampton, Va
“Pseudo-time method for optimal shape design using the Euler equations” Subjects and Themes:
- Subjects: ➤ Euler equations of motion - Computational fluid dynamics - Optimization - Algorithms - Compressible flow - Aerodynamic configurations - Computer aided design
Edition Identifiers:
- The Open Library ID: OL17141224M - OL15425896M - OL18088570M - OL19004098M
- Online Computer Library Center (OCLC) ID: 35518438
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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9Navier-Stokes simulation of several high-lift reference H configurations
By Wendy B. Lessard
“Navier-Stokes simulation of several high-lift reference H configurations” Metadata:
- Title: ➤ Navier-Stokes simulation of several high-lift reference H configurations
- Author: Wendy B. Lessard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - Hampton, Va - Hanover, MD
“Navier-Stokes simulation of several high-lift reference H configurations” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Angle of attack - Body-wing configurations - Computational fluid dynamics - Navier-Stokes equation - Reynolds number - Structured grids (Mathematics) - Supersonic speed - Supersonic transports - Vortices - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15569338M - OL18140130M - OL18296120M - OL17595527M
- Online Computer Library Center (OCLC) ID: 44441535
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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10The lift-fan aircraft
By W. H. Deckert
“The lift-fan aircraft” Metadata:
- Title: The lift-fan aircraft
- Author: W. H. Deckert
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“The lift-fan aircraft” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aircraft design - Flight simulation - Lift fans - Propulsion - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17017590M - OL15413716M - OL18081172M
- Online Computer Library Center (OCLC) ID: 33394644
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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11Supersonic wing and wing-body shape optimization using an adjoint formulation
By James Reuther
“Supersonic wing and wing-body shape optimization using an adjoint formulation” Metadata:
- Title: ➤ Supersonic wing and wing-body shape optimization using an adjoint formulation
- Author: James Reuther
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Moffett Field, Calif.]
“Supersonic wing and wing-body shape optimization using an adjoint formulation” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic aircraft - Body-wing configurations - Supersonic flow - Three dimensional flow - Control theory - Optimization - Euler equations of motion - Aerodynamic configurations - Aircraft design - Wings - Supersonic airfoils
Edition Identifiers:
- The Open Library ID: OL18084750M - OL15419682M - OL17076145M
- Online Computer Library Center (OCLC) ID: 34762339
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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12Wing-section optimization for supersonic viscous flow
By Cem C. Item
“Wing-section optimization for supersonic viscous flow” Metadata:
- Title: ➤ Wing-section optimization for supersonic viscous flow
- 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 flow” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Mathematical models - Supersonic flow - Aicraft design - Navier-Stokes equation - Airfoils - Aerodynamic configurations - Two dimensional models - Computer aided design
Edition Identifiers:
- The Open Library ID: OL17078554M - OL18084623M - OL15419484M
- Online Computer Library Center (OCLC) ID: 34608891
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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13Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
By Floyd J. Wilcox
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Metadata:
- Title: ➤ Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6
- Author: Floyd J. Wilcox
- Language: English
- Number of Pages: Median: 43
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - Springfield, VA - [Springfield, VA
“Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamics, Hypersonic - Bombers - Design and construction - External store separation - External stores - Flat plates - Free flow - Hypersonic Aerodynamics - Hypersonic speed - Separated flow
Edition Identifiers:
- The Open Library ID: OL17635043M - OL16125421M - OL17803983M
- Online Computer Library Center (OCLC) ID: 60398151 - 33144596
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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14Design of supersonic transport flap systems for thrust recovery at subsonic speeds
By Michael J. Mann
“Design of supersonic transport flap systems for thrust recovery at subsonic speeds” Metadata:
- Title: ➤ Design of supersonic transport flap systems for thrust recovery at subsonic speeds
- Author: Michael J. Mann
- 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
“Design of supersonic transport flap systems for thrust recovery at subsonic speeds” Subjects and Themes:
- Subjects: Aerodynamic configurations - Design analysis - Flapping - Subsonic speed - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15577761M - OL17597452M
- Online Computer Library Center (OCLC) ID: 45080427
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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15Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
By John D. Berry
“Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight” Metadata:
- Title: ➤ Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight
- Author: John D. Berry
- Language: English
- Number of Pages: Median: 245
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va
“Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamics - Helicopters - Horizontal flight - Rotors (Helicopters) - Separated flow - Testing - Turbulence effects - Unsteady flow - Velocity distribution - Velocity measurment - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL16137805M - OL17595877M
- Online Computer Library Center (OCLC) ID: 39713178
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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16Viper
By L. E. Paul Gilbert
“Viper” Metadata:
- Title: Viper
- Author: L. E. Paul Gilbert
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1993
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Viper” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Training aircraft - Aircraft engines - Laminar flow airfoils - Aerodynamic configurations - Aircraft design
Edition Identifiers:
- The Open Library ID: OL17683421M - OL17788534M
- Online Computer Library Center (OCLC) ID: 32636376
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17HOMAR:a computer code for generating homotopic grids using algebraic relations
By Anutosh Moitra
“HOMAR:a computer code for generating homotopic grids using algebraic relations” Metadata:
- Title: ➤ HOMAR:a computer code for generating homotopic grids using algebraic relations
- Author: Anutosh Moitra
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“HOMAR:a computer code for generating homotopic grids using algebraic relations” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aircraft configurations - Applications programs (Computers) - Body-wing configurations - Computational geometry - Computational grids - Computer systems programs - Grid generation (Matematics) - Homotopy theory
Edition Identifiers:
- The Open Library ID: OL14972278M - OL17683520M
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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18Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
By Christopher A. Lee
“Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport” Metadata:
- Title: ➤ Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
- Author: Christopher A. Lee
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ San Jose, CA - Springfield, Va - [Washington, DC
“Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Canard configurations - Design analysis - Performance tests - Sonic booms - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15413726M - OL17791642M
- Online Computer Library Center (OCLC) ID: 33431926
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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19A 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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20Wing-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
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21Experimental aerothermodynamic research of hypersonic aircraft
By Joseph W. Cleary
“Experimental aerothermodynamic research of hypersonic aircraft” Metadata:
- Title: ➤ Experimental aerothermodynamic research of hypersonic aircraft
- Author: Joseph W. Cleary
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987 - 1989
- Publish Location: ➤ Springfield, Va.? - [Washington, DC
“Experimental aerothermodynamic research of hypersonic aircraft” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Pressure distribution - Afterbodies - Forebodies - Flow distribution - Aerothermodynamics - Hypersonic aircraft - Wind tunnel models - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL15398951M - OL15408376M
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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22Three-dimensional aerodynamic shape optimization of supersonic delta wings
By Gregory Wayne Burgreen
“Three-dimensional aerodynamic shape optimization of supersonic delta wings” Metadata:
- Title: ➤ Three-dimensional aerodynamic shape optimization of supersonic delta wings
- Author: Gregory Wayne Burgreen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - American Institute of Aeronautics and Astornautics - [National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Washington, D.C
“Three-dimensional aerodynamic shape optimization of supersonic delta wings” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Three dimensional models - Sensitivity - Applications programs (Computers) - Design analysis - Discrete functions - Aerodynamic configurations - Aircraft design - Multidisciplinary design optimization
Edition Identifiers:
- The Open Library ID: OL15419480M - OL18084613M
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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23Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
By Gregory Wayne Burgreen
“Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” Metadata:
- Title: ➤ Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
- Author: Gregory Wayne Burgreen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic nozzles - Sensitivity - Delta wings - Discrete functions - Airfoils - Aerodynamic configurations - Aircraft design - Supercritical wings - Computer aided design
Edition Identifiers:
- The Open Library ID: OL15419545M - OL18084662M
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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24Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
By Zachary T. Applin
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:
- Title: ➤ Pressure distributions from subsonic tests of a NACA 0012 semispan wing 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
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Airfoil profiles - Dynamic pressure - Free flow - Pressure distribution - Semispan models - Subsonic speed - Unswept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15421506M - OL17794166M
- Online Computer Library Center (OCLC) ID: 35231688
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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25Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids
By J. C. Newman
“Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids” Metadata:
- Title: ➤ Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids
- Author: J. C. Newman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids” Subjects and Themes:
- Subjects: ➤ Differential equations - Optimization - Boeing 747 aircraft - Conjugate gradient method - Aerodynamic configurations - Parameterization - Finite volume method
Edition Identifiers:
- The Open Library ID: OL15509269M - OL17837675M
- Online Computer Library Center (OCLC) ID: 40510901
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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26The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows
By Darshan Dosanjh
“The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows” Metadata:
- Title: ➤ The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows
- Author: Darshan Dosanjh
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows” Subjects and Themes:
- Subjects: ➤ Temperature effects - Aeronautical engineering - Jet flow - Performance tests - Coaxial nozzles - Acoustic properties - Pressure ratio - Aerodynamic configurations - Nozzle design - Gas expansion - Noise reduction
Edition Identifiers:
- The Open Library ID: OL17017656M - OL17683982M
- Online Computer Library Center (OCLC) ID: 33901750
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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27A Two element laminar flow airfoil optimized for cruise
By Gregory Glen Steen
“A Two element laminar flow airfoil optimized for cruise” Metadata:
- Title: ➤ A Two element laminar flow airfoil optimized for cruise
- Author: Gregory Glen Steen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Texas A&M University - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [College Station, TX?] - [Washington, DC - Springfield, Va
“A Two element laminar flow airfoil optimized for cruise” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamic drag - Aircraft design - Airfoils - Cruising flight - Laminar flow - Lift - Lift drag ratio - Wind tunnel tests - Wings
Edition Identifiers:
- The Open Library ID: OL15414633M - OL17792073M
- Online Computer Library Center (OCLC) ID: 34053955
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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28Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions
By Luc Huyse
“Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions” Metadata:
- Title: ➤ Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions
- Author: Luc Huyse
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, VA - Springfield, VA
“Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Airfoils - Optimization - Robustness (Mathematics) - Statistical analysis - Two dimensional models
Edition Identifiers:
- The Open Library ID: OL16012144M
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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29Development of an automatic grid generator for multi-element high-lift wings
By Scott Eberhardt
“Development of an automatic grid generator for multi-element high-lift wings” Metadata:
- Title: ➤ Development of an automatic grid generator for multi-element high-lift wings
- Author: Scott Eberhardt
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Development of an automatic grid generator for multi-element high-lift wings” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Computational grids - Grid generation (Mathematics) - Laplace equation - Predictor-corrector methods - Wings
Edition Identifiers:
- The Open Library ID: OL15485877M
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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30Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis
By Oktay Baysal
“Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis” Metadata:
- Title: ➤ Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis
- 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
“Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aircraft design - Algorithms - Computational fluid dynamics - Computer aided design - Design analysis - Optimization - Shapes - Supersonic flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15419489M
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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31High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion
By Bobby L. Berrier
“High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion” Metadata:
- Title: ➤ High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion
- Author: Bobby L. Berrier
- Language: English
- Number of Pages: Median: 165
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2005
- Publish Location: Hampton, Va
“High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion” Subjects and Themes:
- Subjects: Boundary layers - Aerodynamic configurations - Air flow - Ducts - Engine inlets
Edition Identifiers:
- The Open Library ID: OL43928567M
- Online Computer Library Center (OCLC) ID: 793417465
Access and General Info:
- First Year Published: 2005
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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32Three dimensional grid generation for complex configurations - recent progress
By Joe F. Thompson
“Three dimensional grid generation for complex configurations - recent progress” Metadata:
- Title: ➤ Three dimensional grid generation for complex configurations - recent progress
- Author: Joe F. Thompson
- Number of Pages: Median: 153
- Publisher: AGARD
- Publish Date: 1988
- Publish Location: Neuilly sur Seine, France
“Three dimensional grid generation for complex configurations - recent progress” Subjects and Themes:
- Subjects: Aerodynamic configurations - Grids
Edition Identifiers:
- The Open Library ID: OL18926892M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Special course on aircraft dynamics at high angles of attack: experiments and modelling
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Special course on aircraft dynamics at high angles of attack: experiments and modelling” Metadata:
- Title: ➤ Special course on aircraft dynamics at high angles of attack: experiments and modelling
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Number of Pages: Median: 144
- Publisher: AGARD
- Publish Date: 1991
- Publish Location: Neuilly sur Seine, France
“Special course on aircraft dynamics at high angles of attack: experiments and modelling” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL21499310M
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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34Advanced Rotorcraft Transmission Program
By Robert C. Bill
“Advanced Rotorcraft Transmission Program” Metadata:
- Title: ➤ Advanced Rotorcraft Transmission Program
- Author: Robert C. Bill
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1990
- Publish Location: [Cleveland, Ohio
“Advanced Rotorcraft Transmission Program” Subjects and Themes:
- Subjects: ➤ Helicopter design - Helicopter propeller drive - Mechanical drives - Aircraft configurations - Rotary wing aircraft - Transmissions (Machine elements) - Noise reduction - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL16131237M
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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35Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor
By Arthur E. Phelps
“Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor” Metadata:
- Title: ➤ Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor
- Author: Arthur E. Phelps
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, DC]
“Effects of planform geometry on hover performance of a 2-meter-diameter model of a four-bladed rotor” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Blades - Hovering - Rotor blades (Turbomachinery) - Rotors (Helicopters) - Structural design criteria - Turbomachines
Edition Identifiers:
- The Open Library ID: OL17727205M
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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36Aerodynamic optimization by simultaneously updating flow variables and design parameters with application to advanced propeller designs
By Magdi H. Rizk
“Aerodynamic optimization by simultaneously updating flow variables and design parameters with application to advanced propeller designs” Metadata:
- Title: ➤ Aerodynamic optimization by simultaneously updating flow variables and design parameters with application to advanced propeller designs
- Author: Magdi H. Rizk
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Aerodynamic optimization by simultaneously updating flow variables and design parameters with application to advanced propeller designs” Subjects and Themes:
- Subjects: ➤ Variability - Optimization - Aerodynamic configurations - Fluid flow - Propellers - Design analysis
Edition Identifiers:
- The Open Library ID: OL15407462M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Study of the integration of wind tunnel and computational methods for aerodynamic configurations
By Lindsay E. Browne
“Study of the integration of wind tunnel and computational methods for aerodynamic configurations” Metadata:
- Title: ➤ Study of the integration of wind tunnel and computational methods for aerodynamic configurations
- Author: Lindsay E. Browne
- Language: English
- Number of Pages: Median: 66
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1989
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Study of the integration of wind tunnel and computational methods for aerodynamic configurations” Subjects and Themes:
- Subjects: ➤ Wind tunnel walls - Computational fluid dynamics - Panel method (Fluid dynamics) - Aerodynamics - Wind tunnel tests - Flow distribution - Wall flow - Mathematical models - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL16138511M
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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38Implementation of a multiblock sensitivity analysis method in numerical aerodynamic shape optimization
By James M. Lacasse
“Implementation of a multiblock sensitivity analysis method in numerical aerodynamic shape optimization” Metadata:
- Title: ➤ Implementation of a multiblock sensitivity analysis method in numerical aerodynamic shape optimization
- Author: James M. Lacasse
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Implementation of a multiblock sensitivity analysis method in numerical aerodynamic shape optimization” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Multigrid methods - Supercritical airfoils - Sensitivity - Navier-Stokes equation - Decomposition - Trajectory optimization - Aerodynamic configurations - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15419542M
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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39An aerodynamic tradeoff study of the scissor wing configuration
By Bruce P. Selberg
“An aerodynamic tradeoff study of the scissor wing configuration” Metadata:
- Title: ➤ An aerodynamic tradeoff study of the scissor wing configuration
- Author: Bruce P. Selberg
- Language: English
- Publisher: ➤ University of Missouri-Rolla - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ Springfield, Va - [Hampton, Va - Rolla, Mo
“An aerodynamic tradeoff study of the scissor wing configuration” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Lift drag ratio - Design and construction - Aircraft stability - Supersonic flight - Aerofoils - Aerodynamic configurations - Variable sweep wings
Edition Identifiers:
- The Open Library ID: OL16128718M
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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40System synthesis in preliminary aircraft design using statistical methods
By Daniel DeLaurentis
“System synthesis in preliminary aircraft design using statistical methods” Metadata:
- Title: ➤ System synthesis in preliminary aircraft design using statistical methods
- Author: Daniel DeLaurentis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“System synthesis in preliminary aircraft design using statistical methods” Subjects and Themes:
- Subjects: ➤ Statistical analysis - Experiment design - Aerodynamic configurations - Probability theory - Aircraft design - Multidisciplinary design optimization - Propulsion system configurations
Edition Identifiers:
- The Open Library ID: OL15543332M
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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41Full potential methods for analysis/design of complex aerospace configurations
By Vijaya Shankar
“Full potential methods for analysis/design of complex aerospace configurations” Metadata:
- Title: ➤ Full potential methods for analysis/design of complex aerospace configurations
- Author: Vijaya Shankar
- Language: English
- Publisher: ➤ Rockwell International Corp. - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Los Angeles, Calif
“Full potential methods for analysis/design of complex aerospace configurations” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamics, Supersonic - Aircraft design - Aircraft maneuvers - Airplanes - Design - Design analysis - Mathematical models - Potential theory - Potential theory (Mathematics) - Supersonic Aerodynamics - Wind tunnel tests - Wings
Edition Identifiers:
- The Open Library ID: OL17724920M
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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42Wing-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: ➤ Computational fluid dynamics - Inviscid flow - Viscous flow - Supersonic flow - Aicraft design - Applications programs (Computers) - Aerodynamic characteristics - Optimization - Airfoils - Aerodynamic configurations - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15419486M
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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43Supersonic civil airplane study and design
By Samson H. Cheung
“Supersonic civil airplane study and design” Metadata:
- Title: ➤ Supersonic civil airplane study and design
- Author: Samson H. Cheung
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ San Jose, CA - Springfield, Va - [Washington, DC
“Supersonic civil airplane study and design” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Computational fluid dynamics - Aircraft configurations - Computer aided design - Sonic booms - Aerodynamic configurations - Aircraft design - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15413728M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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44Aerothermodynamic measurement and prediction for modified orbiter at Mach 6 and 10
By John R. Micol
“Aerothermodynamic measurement and prediction for modified orbiter at Mach 6 and 10” Metadata:
- Title: ➤ Aerothermodynamic measurement and prediction for modified orbiter at Mach 6 and 10
- Author: John R. Micol
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Washington, DC
“Aerothermodynamic measurement and prediction for modified orbiter at Mach 6 and 10” Subjects and Themes:
- Subjects: ➤ Heat transfer - Reynolds number - Wind tunnel tests - Heat measurement - Angle of attack - Aerothermodynamics - Aerodynamic configurations - Mach number
Edition Identifiers:
- The Open Library ID: OL15501804M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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45Sensitivity analysis and optimization of aerodynamic configurations with blend surfaces
By A. M. Thomas
“Sensitivity analysis and optimization of aerodynamic configurations with blend surfaces” Metadata:
- Title: ➤ Sensitivity analysis and optimization of aerodynamic configurations with blend surfaces
- Author: A. M. Thomas
- Language: English
- Publisher: ➤ Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University - National Aeronautics and Space Administration - National Technical Information Service, distributor - Old Dominion University Research Foundation
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Norfolk, Va - Springfield, Va
“Sensitivity analysis and optimization of aerodynamic configurations with blend surfaces” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Sensitivity - Unstructured grids (Mathematics) - Computer systems programs - Design analysis
Edition Identifiers:
- The Open Library ID: OL15479161M
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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46Aeroelasticity of wing and wing-body configurations on parallel computers
By Chansup Byun
“Aeroelasticity of wing and wing-body configurations on parallel computers” Metadata:
- Title: ➤ Aeroelasticity of wing and wing-body configurations on parallel computers
- Author: Chansup Byun
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - MCAT Institute - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - San Jose, CA - [Washington, DC
“Aeroelasticity of wing and wing-body configurations on parallel computers” Subjects and Themes:
- Subjects: ➤ Parallel computers - Body-wing configurations - Aircraft configurations - Parallel processing (Computers) - Computer aided design - Aerodynamic configurations - Aeroelasticity - Aircraft design - Flutter
Edition Identifiers:
- The Open Library ID: OL15413748M
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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47Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model
By Zachary T. Applin
“Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model” Metadata:
- Title: ➤ Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model
- Author: Zachary T. Applin
- Language: English
- Number of Pages: Median: 108
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model” Subjects and Themes:
- Subjects: ➤ Panel method (Fluid dynamics) - Wings - Aerodynamics - Airplanes - Laminar flow - Aerodynamic characteristics - Lift (Aerodynamics) - Boundary layer control - Aerodynamic configurations - Computer programs - Airfoil profiles - Semispan models - Laminar boundary flow
Edition Identifiers:
- The Open Library ID: OL17726185M
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:
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48Water tunnel flow visualization study through poststall of 12 novel planform shapes
By Gregory M. Gatlin
“Water tunnel flow visualization study through poststall of 12 novel planform shapes” Metadata:
- Title: ➤ Water tunnel flow visualization study through poststall of 12 novel planform shapes
- Author: Gregory M. Gatlin
- 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
“Water tunnel flow visualization study through poststall of 12 novel planform shapes” Subjects and Themes:
- Subjects: ➤ Planforms - Water tunnel tests - Flow visualization - Aerodynamic configurations - Free flow - Wing profiles - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15503578M
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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49Analysis of flight data from a high-incidence research model by system identification methods
By James G. Batterson
“Analysis of flight data from a high-incidence research model by system identification methods” Metadata:
- Title: ➤ Analysis of flight data from a high-incidence research model by system identification methods
- Author: James G. Batterson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Analysis of flight data from a high-incidence research model by system identification methods” Subjects and Themes:
- Subjects: ➤ Flight characteristics - Dynamic control - Aerodynamic configurations - Stability derivatives - Aerodynamic stability - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15402324M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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50Aerodynamic analysis of a modified, pylon-mounted JSOW
By Boaz Pomerantz
“Aerodynamic analysis of a modified, pylon-mounted JSOW” Metadata:
- Title: ➤ Aerodynamic analysis of a modified, pylon-mounted JSOW
- Author: Boaz Pomerantz
- Language: English
- Number of Pages: Median: 150
- Publisher: ➤ Available from National Technical Information Service - Naval Postgraduate School
- Publish Date: 1997
- Publish Location: ➤ Monterey, Calif - Springfield, Va
“Aerodynamic analysis of a modified, pylon-mounted JSOW” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL25310659M
- Online Computer Library Center (OCLC) ID: 640487993
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
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- Borrowing from Open Library: Borrowing link
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