Explore: Aerodynamic Stability
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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
Online Access
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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
Online Access
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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:
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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:
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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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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Atmospheric entry
half-angle and properly placed center of mass, a sphere-cone can provide aerodynamic stability from Keplerian entry to surface impact. (The half-angle is the angle
Rifling
firearms's barrel for imparting a spin to a projectile to improve its aerodynamic stability and accuracy. It is also the term (as a verb) for creating such
Relaxed stability
aircraft is said to have relaxed stability if it has low or negative stability. An aircraft with negative stability will have a tendency to change its
Aerodynamics
eighteenth century, although observations of fundamental concepts such as aerodynamic drag were recorded much earlier. Most of the early efforts in aerodynamics
Aircraft flight dynamics
physical situation and is called Prandtl–Glauert singularity. see Aerodynamic force Stability is the ability of the aircraft to counteract disturbances to
Structural integrity and failure
(2001). In the Wake of Tacoma: Suspension Bridges and the Quest for Aerodynamic Stability. ASCE Publications. p. 139. ISBN 0-7844-0542-5. K. Billah and R
Wing configuration
are the low wing loading and high wetted area needed to obtain aerodynamic stability. Variants are: Tailless delta: a classic high-speed design, used
BASE jumping
at lower speeds, have less aerodynamic control. The attitude of the body at the moment of jumping determines the stability of flight in the first few
Strait of Messina Bridge
Structurae. The greatest problem in designing the bridge is the aerodynamic stability of the deck under wind as well as seismic activity. Sabelli, Chiara
Chord (aeronautics)
various wing shapes, the mean aerodynamic chord (abbreviated MAC) is used, although it is complex to calculate. The mean aerodynamic chord is used for calculating