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Source: The Open Library
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11999 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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2Evaluation 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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3Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
By G. Guruswamy
“Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” Metadata:
- Title: ➤ Euler/Navier-Stokes flow computations on flexible configurations for stability analysis
- Author: G. Guruswamy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, American Institute of Aeronautics and Astronautics
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Euler/Navier-Stokes flow computations on flexible configurations for stability analysis” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Structured grids (Mathematics) - Turbulence models - Finite difference theory - Aerodynamic stability - Navier-Stokes equation - Longitudinal stability - Stability derivatives - Angle of attack - Mach number
Edition Identifiers:
- The Open Library ID: OL17122527M - OL15452312M - OL17573079M - OL18100861M
- Online Computer Library Center (OCLC) ID: 38733169
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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4Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
By Scott P. Fears
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
- Author: Scott P. Fears
- Language: English
- Number of Pages: Median: 145
- Publisher: ➤ National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - [Washington, DC - Springfield, Va
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Aspect ratio - Flight stability tests - Stabilizers (Fluid dynamics) - Wind tunnel tests - Wing profiles - Aerodynamic stability - Angle of attack - Stability - Flight control - Low speed - Planforms - Arrow wings - Tail assemblies - Leading edge flaps
Edition Identifiers:
- The Open Library ID: OL19003591M - OL15416719M - OL18082907M - OL17032232M
- Online Computer Library Center (OCLC) ID: 34127880
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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5Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
By Glen P. Doggett
“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Metadata:
- Title: ➤ Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
- Author: Glen P. Doggett
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, Va
“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Hypersonics - Aerodynamic stability - Navier-Stokes equation - Hypersonic boundary layer - Hypersonic speed - Aerodynamic noise - Zero angle of attack - Angle of attack
Edition Identifiers:
- The Open Library ID: OL18114813M - OL15487085M - OL17123234M - OL17564495M
- Online Computer Library Center (OCLC) ID: 38994217
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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6The 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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7Low-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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8Performance of a low-power subsonic-arc-attachment arcjet thruster
By John M. Sankovic
“Performance of a low-power subsonic-arc-attachment arcjet thruster” Metadata:
- Title: ➤ Performance of a low-power subsonic-arc-attachment arcjet thruster
- Author: John M. Sankovic
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - NASA
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Performance of a low-power subsonic-arc-attachment arcjet thruster” Subjects and Themes:
- Subjects: ➤ Flow velocity - Fuel injection - Propulsion system performance - Aerodynamic stability - Specific impulse - Electric propulsion - Rocket engine design - Arc jet engines
Edition Identifiers:
- The Open Library ID: OL17117082M - OL18085535M - OL15420784M - OL17794628M
- Online Computer Library Center (OCLC) ID: 34778391
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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9Full-scale hingeless rotor performance and loads
By Randall L. Peterson
“Full-scale hingeless rotor performance and loads” Metadata:
- Title: ➤ Full-scale hingeless rotor performance and loads
- Author: Randall L. Peterson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Full-scale hingeless rotor performance and loads” Subjects and Themes:
- Subjects: ➤ 80-105 helicopter - Aerodynamic loads - Aerodynamic stability - Aeroelasticity - Data bases - Databases - Full scale tests - Rigid rotors - Rotating shafts - Rotor aerodynamics - Rotor blades - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL17070226M - OL17117614M - OL18086109M - OL15421543M
- Online Computer Library Center (OCLC) ID: 35216887
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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10Low-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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11Nonlinear stability of supersonic jets
By R. S. Bhatt
“Nonlinear stability of supersonic jets” Metadata:
- Title: ➤ Nonlinear stability of supersonic jets
- Author: R. S. Bhatt
- Language: English
- Publisher: ➤ NASA Langley Research Center - Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995 - 1996
- Publish Location: ➤ Springfield, Va - Norfolk, Va - Hampton, Va - [Springfield, Va - [Washington, DC
“Nonlinear stability of supersonic jets” Subjects and Themes:
- Subjects: ➤ Aerodynamic noise - Aerodynamic stability - Aircraft structures - Jet aircraft noise - Linearity - Navier-Stokes equation - Noise reduction - Nonlinearity - Operating temperature - Parabolic Differential equations - Parallel flow - Rayleigh equations - Shock waves - Supersonic commercial air transport - Supersonic jet flow
Edition Identifiers:
- The Open Library ID: OL17130773M - OL17125173M
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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12Aeroelastic stability of a full-scale hingeless rotor
By Randall L. Peterson
“Aeroelastic stability of a full-scale hingeless rotor” Metadata:
- Title: ➤ Aeroelastic stability of a full-scale hingeless rotor
- Author: Randall L. Peterson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Aeroelastic stability of a full-scale hingeless rotor” Subjects and Themes:
- Subjects: ➤ Rotor lift - Rotary wings - Loads (Forces) - Shafts (Machine elements) - Aerodynamic stability - BO-105 helicopter - Hovering - Rigid rotors - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL15498159M - OL17834422M
- Online Computer Library Center (OCLC) ID: 39705625
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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13A spectrally accurate boundary-layer code for infinite swept wings
By C. David Pruett
“A spectrally accurate boundary-layer code for infinite swept wings” Metadata:
- Title: ➤ A spectrally accurate boundary-layer code for infinite swept wings
- Author: C. David Pruett
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“A spectrally accurate boundary-layer code for infinite swept wings” Subjects and Themes:
- Subjects: ➤ Aerodynamic stability - Backward differencing - Boundary conditions - Boundary layer equations - Compressible boundary layer - Spectral methods - Swept wings - Three dimensional boundary layer
Edition Identifiers:
- The Open Library ID: OL15409684M - OL17790947M
- Online Computer Library Center (OCLC) ID: 32799476
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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14Aerothermodynamics of the Mars Global Surveyor spacecraft
By Russell W. Shane
“Aerothermodynamics of the Mars Global Surveyor spacecraft” Metadata:
- Title: ➤ Aerothermodynamics of the Mars Global Surveyor spacecraft
- Author: Russell W. Shane
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Aerothermodynamics of the Mars Global Surveyor spacecraft” Subjects and Themes:
- Subjects: ➤ Aerodynamic heating - Aerodynamic stability - Aerothermodynamics - Monte Carlo method - Three dimensional models - Transition flow
Edition Identifiers:
- The Open Library ID: OL17597467M - OL15547936M
- Online Computer Library Center (OCLC) ID: 42321700
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15FPCAS3D user's guide
By Milind A. Bakhle
“FPCAS3D user's guide” Metadata:
- Title: FPCAS3D user's guide
- Author: Milind A. Bakhle
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“FPCAS3D user's guide” Subjects and Themes:
- Subjects: ➤ Unsteady aerodynamics - User manuals (Computer programs) - Flutter analysis - Applications programs (Computers) - Aerodynamic stability - Aeroelasticity - Flutter - Finite element method
Edition Identifiers:
- The Open Library ID: OL15414978M - OL17792146M
- Online Computer Library Center (OCLC) ID: 33973418
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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16Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
By Vladislav Klein
“Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” Metadata:
- Title: ➤ Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
- Author: Vladislav Klein
- 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
“Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic stability - Lift - Longitudinal stability - Pitching moments - Uunsteady aerodynamics - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15559425M
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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17Direct adaptive aircraft control using dynamic cell structure neural networks
By Charles C. Jorgensen
“Direct adaptive aircraft control using dynamic cell structure neural networks” Metadata:
- Title: ➤ Direct adaptive aircraft control using dynamic cell structure neural networks
- Author: Charles C. Jorgensen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Direct adaptive aircraft control using dynamic cell structure neural networks” Subjects and Themes:
- Subjects: ➤ Adaptive control - Aerodynamic stability - Aircraft design - F-15 aircraft - Neural nets - On-line systems - Real time operation - Virtual reality
Edition Identifiers:
- The Open Library ID: OL15542968M
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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18Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method
By M. Napolitano
“Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method” Metadata:
- Title: ➤ Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method
- Author: M. Napolitano
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - West Virginia University
- Publish Date: 1995
- Publish Location: ➤ Morgantown, WV - [Washington, DC - Springfield, Va
“Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method” Subjects and Themes:
- Subjects: ➤ Aerodynamic stability - Aircraft control - Equations of state - Lateral control - Longitudinal control - Maximum likelihood estimates - Research vehicles
Edition Identifiers:
- The Open Library ID: OL17683515M
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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19Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
By Bobby W. Sanders
“Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” Metadata:
- Title: ➤ Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
- Author: Bobby W. Sanders
- Language: English
- Number of Pages: Median: 98
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1980
- Publish Location: Washington, D.C
“Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” Subjects and Themes:
- Subjects: ➤ Airplanes - Turbojet engines - Air intakes - Motors - Valves - Aerodynamic stability - Bypasses - Propulsion system performance - Supersonic inlets - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL43506459M
- Online Computer Library Center (OCLC) ID: 761221787
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Identification of dynamic systems - applications to aircraft
By Richard E. Maine
“Identification of dynamic systems - applications to aircraft” Metadata:
- Title: ➤ Identification of dynamic systems - applications to aircraft
- Author: Richard E. Maine
- Publisher: AGARD
- Publish Date: 1986
- Publish Location: Neuilly sur Seine, France
“Identification of dynamic systems - applications to aircraft” Subjects and Themes:
- Subjects: ➤ Aerodynamic stability - Data processing - Flight characteristics - Flight control - Flight paths - Flight test instruments - Flight tests
Edition Identifiers:
- The Open Library ID: OL18998417M
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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21Static aeroelasticity in combat aircraft
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Static aeroelasticity in combat aircraft” Metadata:
- Title: ➤ Static aeroelasticity in combat aircraft
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Publisher: AGARD
- Publish Date: 1986
- Publish Location: Neuilly sur Seine, France
“Static aeroelasticity in combat aircraft” Subjects and Themes:
- Subjects: Aerodynamic stability - Aeroelasticity - Fighter aircraft - Flight control
Edition Identifiers:
- The Open Library ID: OL19986513M
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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22CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft
By Michael B. Lance
“CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft” Metadata:
- Title: ➤ CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft
- Author: Michael B. Lance
- 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
“CLMNANAL, a C++ program for application of the Coleman stability analysis to rotorcraft” Subjects and Themes:
- Subjects: Ground resonance - Rotary wing aircraft - Aerodynamic stability - Applications programs (Computers)
- People: R. P. Coleman - A. M. Feingold
Edition Identifiers:
- The Open Library ID: OL15452325M
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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23Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
By G. H. Gaonkar
“Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Metadata:
- Title: ➤ Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
- Author: G. H. Gaonkar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
- Publish Date: 1994
- Publish Location: ➤ Boca Raton, FL - Springfield, Va - [Washington, DC
“Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic drag - Wakes - Aerodynamic stalling - Torsional vibration - Aeroelasticity - Aerodynamic stability
Edition Identifiers:
- The Open Library ID: OL17029328M
- Online Computer Library Center (OCLC) ID: 32035217
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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24Effect of control surface mass unbalance on the stability of a closed-loop active control system
By E. Nissim
“Effect of control surface mass unbalance on the stability of a closed-loop active control system” Metadata:
- Title: ➤ Effect of control surface mass unbalance on the stability of a closed-loop active control system
- Author: E. Nissim
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effect of control surface mass unbalance on the stability of a closed-loop active control system” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Feedback control - Aerodynamic stability - Flutter - Mass distribution - Control surfaces - Balance - Inertia - Active control
Edition Identifiers:
- The Open Library ID: OL15402406M
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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25Analysis 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
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26Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
By A. M. Springer
“Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Metadata:
- Title: ➤ Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
- Author: A. M. Springer
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 1995
- Publish Location: [Springfield, Va - MSFC, Ala
“Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Subjects and Themes:
- Subjects: ➤ Body-wing configurations - Aerodynamic characteristics - Wind tunnel tests - Longitudinal stability - Subsonic speed - Aerodynamic stability - Angle of attack - Single stage to orbit vehicles - Sideslip - Aerodynamic forces - Lateral stability - Control surfaces - Transonic speed - Mach number - Spacecraft stability
Edition Identifiers:
- The Open Library ID: OL15416729M
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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27Subsonic wing optimization for handling qualities using ACSYNT
By Dani Soban
“Subsonic wing optimization for handling qualities using ACSYNT” Metadata:
- Title: ➤ Subsonic wing optimization for handling qualities using ACSYNT
- Author: Dani Soban
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Subsonic wing optimization for handling qualities using ACSYNT” Subjects and Themes:
- Subjects: ➤ Aircraft stability - Three dimensional models - Applications programs (Computers) - Vortex lattice method - Aerodynamic stability - Computer aided design
Edition Identifiers:
- The Open Library ID: OL15507258M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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28Euler technology assessment
By Keith J. Jordan
“Euler technology assessment” Metadata:
- Title: Euler technology assessment
- Author: Keith J. Jordan
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - Springfield, VA
“Euler technology assessment” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Viscous flow - Fighter aircraft - Turbulent flow - Unstructured grids (Mathematics) - Finite volume method - Aerodynamic stability - Navier-Stokes equation - Inviscid flow - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15547306M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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29Theory of aerodynamic instability and the mechanism of flutter
By Theodore Theodorsen
“Theory of aerodynamic instability and the mechanism of flutter” Metadata:
- Title: ➤ Theory of aerodynamic instability and the mechanism of flutter
- Author: Theodore Theodorsen
- Number of Pages: Median: 23
- Publisher: NACA
- Publish Date: 1935
- Publish Location: Washington
“Theory of aerodynamic instability and the mechanism of flutter” Subjects and Themes:
- Subjects: Flutter - Aerodynamic stability
Edition Identifiers:
- The Open Library ID: OL19379581M
Access and General Info:
- First Year Published: 1935
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Rotorcraft dynamics 1984
By Specialists' Meeting on Rotorcraft Dynamics (2nd 1984 Ames Research Center)
“Rotorcraft dynamics 1984” Metadata:
- Title: Rotorcraft dynamics 1984
- Author: ➤ Specialists' Meeting on Rotorcraft Dynamics (2nd 1984 Ames Research Center)
- Language: English
- Number of Pages: Median: 501
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Rotorcraft dynamics 1984” Subjects and Themes:
- Subjects: ➤ Congresses - Aerodynamics - Helicopters - Helicopter design - Vibration - Aerodynamic loads - Helicopter performance - Aerodynamic stability - Rotary wing aircraft - Stability of helicopters - Rotors (Helicopters)
Edition Identifiers:
- The Open Library ID: OL14544076M
- Online Computer Library Center (OCLC) ID: 17512066
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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31The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206
By Jaap H. de Leeuw
“The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206” Metadata:
- Title: ➤ The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206
- Author: Jaap H. de Leeuw
- Number of Pages: Median: 54
- Publisher: ➤ National Research Council Canada
- Publish Date: 1987
- Publish Location: Ottawa
“The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206” Subjects and Themes:
- Subjects: ➤ Helicopters - Flight stability tests - Bell 205 helicopter - Parameter identification - Bell 206 helicopter - Aerodynamic stability
Edition Identifiers:
- The Open Library ID: OL19252103M
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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32Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
“Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft” Metadata:
- Title: ➤ Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1999
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft” Subjects and Themes:
- Subjects: ➤ F-18 aircraft - Compressors - Subsonic speed - Aerodynamic stability - Angle of attack - Flight control - Research vehicles - Rotors - Control surfaces
Edition Identifiers:
- The Open Library ID: OL17839405M
- Online Computer Library Center (OCLC) ID: 41964667
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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33Design of robust suboptimal controllers for a generalized quadratic criterion
By Kurtis Brett Miller
“Design of robust suboptimal controllers for a generalized quadratic criterion” Metadata:
- Title: ➤ Design of robust suboptimal controllers for a generalized quadratic criterion
- Author: Kurtis Brett Miller
- Language: English
- Number of Pages: Median: 57
- Publisher: ➤ Naval Postgraduate School - Available from National Technical Information Service
- Publish Date: 1992
- Publish Location: ➤ Monterey, Calif - Springfield, Va
“Design of robust suboptimal controllers for a generalized quadratic criterion” Subjects and Themes:
- Subjects: CONTROL SYSTEMS - FIGHTER AIRCRAFT - AERODYNAMIC STABILITY
Edition Identifiers:
- The Open Library ID: OL25525755M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
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- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
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