Explore: Aerodynamic Loads
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Modal analysis of UH-60A instrumented rotor blades
By Karen S. Hamade
“Modal analysis of UH-60A instrumented rotor blades” Metadata:
- Title: ➤ Modal analysis of UH-60A instrumented rotor blades
- Author: Karen S. Hamade
- Language: English
- Number of Pages: Median: 44
- Publisher: ➤ Ames Research Center - 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: ➤ [Washington, D.C.] - Moffett Field, Calif - Springfield, Va
“Modal analysis of UH-60A instrumented rotor blades” Subjects and Themes:
- Subjects: ➤ Rotors (Helicopters) - Aerodynamics - Testing - Computer simulation - Mode (Statistics) - Aerodynamic loads - Rotor aerodynamics - NASTRAN - Rotor blades - Analogies - Finite element method - Rotary wings - UH-60A helicopter
Edition Identifiers:
- The Open Library ID: OL16132235M - OL21334910M - OL17630305M - OL18249916M - OL20571041M
- Online Computer Library Center (OCLC) ID: 48997799
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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2Development of a low-aspect ratio fin for flight research experiments
By David M. Richwine
“Development of a low-aspect ratio fin for flight research experiments” Metadata:
- Title: ➤ Development of a low-aspect ratio fin for flight research experiments
- Author: David M. Richwine
- Language: English
- Number of Pages: Median: 13
- Publisher: ➤ Dryden Flight Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1994
- Publish Location: ➤ Edwards, Calif - [Washington, DC] - [Springfield, Va
“Development of a low-aspect ratio fin for flight research experiments” Subjects and Themes:
- Subjects: ➤ Aerodynamic loads - F-15 aircraft - Fins - Flight test vehicles - Flight tests - Ground tests - Low aspect ratio
Edition Identifiers:
- The Open Library ID: OL16982778M - OL15409599M - OL17114754M - OL19006125M - OL18079157M
- Online Computer Library Center (OCLC) ID: 32789398
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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3Finite element thermo-viscoplastic analysis of aerospace structures
By Ajay K. Pandey
“Finite element thermo-viscoplastic analysis of aerospace structures” Metadata:
- Title: ➤ Finite element thermo-viscoplastic analysis of aerospace structures
- Author: Ajay K. Pandey
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Finite element thermo-viscoplastic analysis of aerospace structures” Subjects and Themes:
- Subjects: ➤ Viscoplasticity - Aircraft structures - Aerodynamic loads - Thermal stresses - Aerodynamic interference - Hypersonic vehicles - Aerothermodynamics - Finite element method - Aerodynamic heating - Leading edges - Thermoelasticity - Plastic deformation - Thermal analysis - Structural analysis
Edition Identifiers:
- The Open Library ID: OL18227548M - OL19146742M - OL17725177M - OL17630485M
- Online Computer Library Center (OCLC) ID: 60361554
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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4A new higher-order composite theory for analysis and design of high speed tilt-rotor blades
By Thomas R. McCarthy
“A new higher-order composite theory for analysis and design of high speed tilt-rotor blades” Metadata:
- Title: ➤ A new higher-order composite theory for analysis and design of high speed tilt-rotor blades
- Author: Thomas R. McCarthy
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“A new higher-order composite theory for analysis and design of high speed tilt-rotor blades” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic loads - Mathematical models - Three dimensional models - Multidisciplinary design optimization - Aeroelasticity - Composite structures - Tilt rotor aircraft
Edition Identifiers:
- The Open Library ID: OL18121419M - OL17572102M - OL15504887M - OL17125882M
- Online Computer Library Center (OCLC) ID: 39949382
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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5Full-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: ➤ [Springfield, Va - Moffett Field, Calif
“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: OL15421543M - OL17117614M - OL18086109M - OL17070226M
- 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
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6Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program
By J. B. Graham
“Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program” Metadata:
- Title: ➤ Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program
- Author: J. B. Graham
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 1998
- Publish Location: ➤ [Marshall Space Flight Center], Ala - [Springfield, Va
“Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program” Subjects and Themes:
- Subjects: ➤ Thrust - Finite element method - Launch vehicles - Aerodynamic loads - Computer programs - Applications programs (Computers)
Edition Identifiers:
- The Open Library ID: OL15541940M - OL18132699M - OL17580357M - OL17130053M
- Online Computer Library Center (OCLC) ID: 41177113
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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7Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
By David S. Dolling
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Metadata:
- Title: ➤ Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
- Author: David S. Dolling
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Austin, Tex - Springfield, Va
“Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Unsteady flow - Boundary layer separation - Aerodynamic loads - Corner flow - Vortex generators - Hypersonic boundary layer - Boundary layer control - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15425915M - OL17803977M - OL18088579M
- Online Computer Library Center (OCLC) ID: 35454133
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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8Aerodynamic interference of high speed ground vehicles
By G. W. Johnston
“Aerodynamic interference of high speed ground vehicles” Metadata:
- Title: ➤ Aerodynamic interference of high speed ground vehicles
- Author: G. W. Johnston
- Publisher: ➤ American Society of Mechanical Engineers - Institute for Aerospace Studies
- Publish Date: 1974 - 1976
- Publish Location: New York - [Downsview, Ont.]
“Aerodynamic interference of high speed ground vehicles” Subjects and Themes:
- Subjects: Aerodynamic interference - Aerodynamic loads - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL19003845M - OL20268536M
Access and General Info:
- First Year Published: 1974
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
By Bruce Charles
“Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” Metadata:
- Title: ➤ Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
- Author: Bruce Charles
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Airfoils - Noise pollution - Aerodynamic loads - Dynamic characteristics - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17591432M - OL15552422M
- Online Computer Library Center (OCLC) ID: 42623818
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Simultaneous optical measurements of axial and tangential steady-state blade deflections
By Anatole P Kurkov
“Simultaneous optical measurements of axial and tangential steady-state blade deflections” Metadata:
- Title: ➤ Simultaneous optical measurements of axial and tangential steady-state blade deflections
- Author: Anatole P Kurkov
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Simultaneous optical measurements of axial and tangential steady-state blade deflections” Subjects and Themes:
- Subjects: ➤ Optical measurement - Centrifugal force - Aerodynamic loads - Wind tunnel tests - Fiber optics - Turbomachinery
Edition Identifiers:
- The Open Library ID: OL17839428M - OL15548973M
- Online Computer Library Center (OCLC) ID: 42045695
Author's Alternative Names:
"Anatole P. Kurkov"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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11Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
By Ken Gee
“Computational analysis of forebody tangential slot blowing on the high alpha research vehicle” Metadata:
- Title: ➤ Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
- Author: Ken Gee
- Language: English
- Publisher: ➤ MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994 - 1995
- Publish Location: ➤ [Washington, DC - San Jose, CA - Springfield, Va
“Computational analysis of forebody tangential slot blowing on the high alpha research vehicle” Subjects and Themes:
- Subjects: ➤ Blowing - Forebodies - Slots - Eddy viscosity - Computational grids - Aerodynamic loads - Research vehicles - Navier-Stokes equation - Transonic flight - F-18 aircraft - Reynolds equation - Directional control - Angle of attack - Yawing moments
Edition Identifiers:
- The Open Library ID: OL18081178M - OL18076388M
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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12Summary of the modeling and test correlations of a NASTRAN finite element vibrations model for the AH-1G helicopter
By J. D. Cronkhite
“Summary of the modeling and test correlations of a NASTRAN finite element vibrations model for the AH-1G helicopter” Metadata:
- Title: ➤ Summary of the modeling and test correlations of a NASTRAN finite element vibrations model for the AH-1G helicopter
- Author: J. D. Cronkhite
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Summary of the modeling and test correlations of a NASTRAN finite element vibrations model for the AH-1G helicopter” Subjects and Themes:
- Subjects: AH-1G helicopter - Aerodynamic loads - Finite element method - NASTRAN - Structural vibration
Edition Identifiers:
- The Open Library ID: OL14985480M - OL17684357M
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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13Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
By Ramadas K. Prabhu
“Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0” Metadata:
- Title: ➤ Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ National Aeronautics and Science Administration, Langley Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Viscous flow - Hypersonic speed - Aerodynamic loads - Supersonic speed - Computational fluid dynamics
Edition Identifiers:
- The Open Library ID: OL17607401M - OL17718834M
- Online Computer Library Center (OCLC) ID: 50134015
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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14Aircraft dynamic loads due to flow separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Aircraft dynamic loads due to flow separation” Metadata:
- Title: ➤ Aircraft dynamic loads due to flow separation
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Language: English
- Number of Pages: Median: 272
- Publisher: AGARD
- Publish Date: 1990
- Publish Location: ➤ Neuilly sur Seine, France - Neuilly-sur-Seine
“Aircraft dynamic loads due to flow separation” Subjects and Themes:
- Subjects: ➤ Aerodynamic load - Aerodynamic loads - Aeroelasticity - Buffeting (Aerodynamics) - Congresses - Separated flow
Edition Identifiers:
- The Open Library ID: OL21334028M - OL20562784M
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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15Aircraft loads due to turbulence and their impact on design and certification
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
“Aircraft loads due to turbulence and their impact on design and certification” Metadata:
- Title: ➤ Aircraft loads due to turbulence and their impact on design and certification
- Author: ➤ North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
- Number of Pages: Median: 100
- Publisher: AGARD
- Publish Date: 1994
- Publish Location: Neuilly sur Seine, France
“Aircraft loads due to turbulence and their impact on design and certification” Subjects and Themes:
- Subjects: Aerodynamic loads - Atmospheric turbulence
Edition Identifiers:
- The Open Library ID: OL19754855M - OL19002991M
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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16Surface pressure measurements on the wing of a wind tunnel model during steady rotation
By Colin A. Martin
“Surface pressure measurements on the wing of a wind tunnel model during steady rotation” Metadata:
- Title: ➤ Surface pressure measurements on the wing of a wind tunnel model during steady rotation
- Author: Colin A. Martin
- Publisher: ➤ Aeronautical Research Laboratory
- Publish Date: 1991
- Publish Location: Melbourne, Australia
“Surface pressure measurements on the wing of a wind tunnel model during steady rotation” Subjects and Themes:
- Subjects: Aerodynamic loads - Aircraft spin - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL21499949M
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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17A CFD/CSD interaction methodology for aircraft wings
By Manoj K. Bhardwaj
“A CFD/CSD interaction methodology for aircraft wings” Metadata:
- Title: ➤ A CFD/CSD interaction methodology for aircraft wings
- Author: Manoj K. Bhardwaj
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“A CFD/CSD interaction methodology for aircraft wings” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Nonlinear systems - Aerodynamic loads - Aerodynamics - Dynamic response - Dynamic structural analysis - Aeroelasticity - Finite element method
Edition Identifiers:
- The Open Library ID: OL15491636M
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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18Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance
By Khanh Q. Nguyen
“Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance” Metadata:
- Title: ➤ Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance
- Author: Khanh Q. Nguyen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance” Subjects and Themes:
- Subjects: ➤ Modal response - Aerodynamic loads - Calibrating - Vibration tests - Rotor aerodynamics - Dampers - Hubs - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15408396M
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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19Higher harmonic control analysis for vibration reduction of helicopter rotor systems
By Khanh Q. Nguyen
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Metadata:
- Title: ➤ Higher harmonic control analysis for vibration reduction of helicopter rotor systems
- Author: Khanh Q. Nguyen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Subjects and Themes:
- Subjects: ➤ Helicopters - Harmonic control - Rotary wings - Matrices (Mathematics) - Aerodynamic loads - Mathematical models - Newton methods - Structural design criteria - Finite element method - Rigid rotors - Vibration damping - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL15408643M
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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20Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects
By Martin R. Waszak
“Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects” Metadata:
- Title: ➤ Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects
- Author: Martin R. Waszak
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects” Subjects and Themes:
- Subjects: Aerodynamic loads - Actuators - Control systems design - Transfer functions - Active control
Edition Identifiers:
- The Open Library ID: OL15544439M
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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21Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips
By K. A. Yuan
“Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips” Metadata:
- Title: ➤ Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips
- Author: K. A. Yuan
- 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
“Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips” Subjects and Themes:
- Subjects: ➤ Dynamic response - Helicopters - Hamiltonian functions - Rotary wings - Aerodynamic loads - Mathematical models - Floquet theorem - Composite structures - Finite element method - Structural analysis - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL15413620M
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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22Development of an apparatus for wind tunnel dynamic experiments at high-Ü
By Nelson Pedreiro
“Development of an apparatus for wind tunnel dynamic experiments at high-Ü” Metadata:
- Title: ➤ Development of an apparatus for wind tunnel dynamic experiments at high-Ü
- Author: Nelson Pedreiro
- Language: English
- Publisher: ➤ Joint Institute for Aeronautics and Acoustics, Stanford University - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Stanford, Calif.]
“Development of an apparatus for wind tunnel dynamic experiments at high-Ü” Subjects and Themes:
- Subjects: ➤ Support systems - Aircraft control - Degrees of freedom - Aerodynamic loads - Wind tunnel tests - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15539602M
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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23Higher harmonic control analysis for vibration reduction of helicopter rotor systems
By Khánh Nguyẽ̂n
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Metadata:
- Title: ➤ Higher harmonic control analysis for vibration reduction of helicopter rotor systems
- Author: Khánh Nguyẽ̂n
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Higher harmonic control analysis for vibration reduction of helicopter rotor systems” Subjects and Themes:
- Subjects: ➤ Helicopters - Harmonic control - Rotary wings - Matrices (Mathematics) - Aerodynamic loads - Mathematical models - Newton methods - Structural design criteria - Finite element method - Rigid rotors - Vibration damping - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17114626M
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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24A numerical model of unsteady, subsonic aeroelastic behavior
By Thomas W. Strganac
“A numerical model of unsteady, subsonic aeroelastic behavior” Metadata:
- Title: ➤ A numerical model of unsteady, subsonic aeroelastic behavior
- Author: Thomas W. Strganac
- Language: English
- Number of Pages: Median: 110
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1987
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“A numerical model of unsteady, subsonic aeroelastic behavior” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Lattices (Mathematics) - Vortices - Aerodynamic loads - Aerodynamics - Research - Equations of motion - Prediction analysis techniques - Mathematical models - Wings
Edition Identifiers:
- The Open Library ID: OL17115126M
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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25Application of higher harmonic control to hingeless rotor systems
By Khánh Nguyẽ̂n
“Application of higher harmonic control to hingeless rotor systems” Metadata:
- Title: ➤ Application of higher harmonic control to hingeless rotor systems
- Author: Khánh Nguyẽ̂n
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
- Publish Date: 1991
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Application of higher harmonic control to hingeless rotor systems” Subjects and Themes:
- Subjects: ➤ Flapping - Harmonic control - Rotary wings - Unsteady aerodynamics - Vibration - Aerodynamic loads - Actuators - Vibratory loads - Finite element method - Rigid rotors - Rotors - Optimal control - Torsion
Edition Identifiers:
- The Open Library ID: OL17115418M
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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26Improvements to the missile aerodynamic prediction code DEMON3
By Marnix F. E. Dillenius
“Improvements to the missile aerodynamic prediction code DEMON3” Metadata:
- Title: ➤ Improvements to the missile aerodynamic prediction code DEMON3
- Author: Marnix F. E. Dillenius
- Number of Pages: Median: 166
- Publisher: Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“Improvements to the missile aerodynamic prediction code DEMON3” Subjects and Themes:
- Subjects: Aerodynamic loads
Edition Identifiers:
- The Open Library ID: OL19243078M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Manual on the flight of flexible aircraft in turbulence
By John C. Houbolt
“Manual on the flight of flexible aircraft in turbulence” Metadata:
- Title: ➤ Manual on the flight of flexible aircraft in turbulence
- Author: John C. Houbolt
- Number of Pages: Median: 160
- Publisher: ➤ Advisory Group for Aerospace Research & Development
- Publish Date: 1991
- Publish Location: Neuilly sur Seine, France
“Manual on the flight of flexible aircraft in turbulence” Subjects and Themes:
- Subjects: Aerodynamic loads - Turbulence - Aircraft design
Edition Identifiers:
- The Open Library ID: OL21499563M
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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28Messung von aerodynamisch bedingten Modellverformungen im Windkanal mittels Moire-Interferometrie
By Peter Helmut Baumann
“Messung von aerodynamisch bedingten Modellverformungen im Windkanal mittels Moire-Interferometrie” Metadata:
- Title: ➤ Messung von aerodynamisch bedingten Modellverformungen im Windkanal mittels Moire-Interferometrie
- Author: Peter Helmut Baumann
- Number of Pages: Median: 125
- Publisher: DLR
- Publish Date: 1994
- Publish Location: Koln, Germany
“Messung von aerodynamisch bedingten Modellverformungen im Windkanal mittels Moire-Interferometrie” Subjects and Themes:
- Subjects: Aerodynamic loads - Moire interferometry
Edition Identifiers:
- The Open Library ID: OL19002394M
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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29An improved computational procedure for the unsteady doublet lattice method
By W. Waldman
“An improved computational procedure for the unsteady doublet lattice method” Metadata:
- Title: ➤ An improved computational procedure for the unsteady doublet lattice method
- Author: W. Waldman
- Number of Pages: Median: 16
- Publisher: ➤ Aeronautical Research Laboratories
- Publish Date: 1986
- Publish Location: Melbourne, Australia
“An improved computational procedure for the unsteady doublet lattice method” Subjects and Themes:
- Subjects: Aerodynamic loads - Computational fluid dynamics - Unsteady flow
Edition Identifiers:
- The Open Library ID: OL19003190M
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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30A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing
By R. H. Landon
“A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing” Metadata:
- Title: ➤ A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing
- Author: R. H. Landon
- Publisher: ➤ Aircraft Research Association Ltd
- Publish Date: 1977
- Publish Location: Manton Lane, Bedford, England
“A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing” Subjects and Themes:
- Subjects: Aerodynamic loads - Aerodynamic stalling - Rotary wings - Helicopters
Edition Identifiers:
- The Open Library ID: OL20966945M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31Rotorcraft 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: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1985
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“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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32Some aspects of aircraft dynamic loads due to flow separation
By D. G. Mabey
“Some aspects of aircraft dynamic loads due to flow separation” Metadata:
- Title: ➤ Some aspects of aircraft dynamic loads due to flow separation
- Author: D. G. Mabey
- Number of Pages: Median: 25
- Publisher: AGARD
- Publish Date: 1988
- Publish Location: Neuilly sur Seine, France
“Some aspects of aircraft dynamic loads due to flow separation” Subjects and Themes:
- Subjects: Aerodynamic loads - Buffeting - Boundary layer separation
Edition Identifiers:
- The Open Library ID: OL20898653M
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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33NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems
By V. Elchuri
“NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems” Metadata:
- Title: ➤ NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems
- Author: V. Elchuri
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1985
- Publish Location: ➤ [Springfield, Va - Cleveland, Ohio
“NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems” Subjects and Themes:
- Subjects: ➤ NASTRAN - Excitation - User manuals (Computer programs) - Aerodynamic loads - Forced vibration - Turbomachinery
Edition Identifiers:
- The Open Library ID: OL15407514M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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34The accuracy of parameter estimation in system identification of noisy aircraft load measurement
By Jeffery Yau-Pak Kong
“The accuracy of parameter estimation in system identification of noisy aircraft load measurement” Metadata:
- Title: ➤ The accuracy of parameter estimation in system identification of noisy aircraft load measurement
- Author: Jeffery Yau-Pak Kong
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration - University of California, Los Angeles
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC - [Los Angeles, Calif.]
“The accuracy of parameter estimation in system identification of noisy aircraft load measurement” Subjects and Themes:
- Subjects: ➤ Aircraft structures - Aerodynamic loads - Estimating - System identification - Noise - Neural nets - Wings - Least squares method
Edition Identifiers:
- The Open Library ID: OL15409378M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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35Determination of stores pointing error due to wing flexibility under flight load
By William A. Lokos
“Determination of stores pointing error due to wing flexibility under flight load” Metadata:
- Title: ➤ Determination of stores pointing error due to wing flexibility under flight load
- Author: William A. Lokos
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Determination of stores pointing error due to wing flexibility under flight load” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Errors - Aerodynamic loads - Elastic deformation - Wing loading - Deflection - Flexibility - Sensors - Wing tanks - Twisted wings
Edition Identifiers:
- The Open Library ID: OL15409389M
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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36System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality
By Ralph David Buehrle
“System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality” Metadata:
- Title: ➤ System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality
- Author: Ralph David Buehrle
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality” Subjects and Themes:
- Subjects: ➤ Wind tunnel models - Unsteady aerodynamics - Equations of motion - Aerodynamic loads - Wind tunnel tests - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15497713M
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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37Aerodynamic limitations of the UH-60A rotor
By Colin P. Coleman
“Aerodynamic limitations of the UH-60A rotor” Metadata:
- Title: ➤ Aerodynamic limitations of the UH-60A rotor
- Author: Colin P. Coleman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Aerodynamic limitations of the UH-60A rotor” Subjects and Themes:
- Subjects: ➤ Pitching moments - UH-60A helicopter - Blade tips - Aerodynamic loads - Rotors - Supercritical flow - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15498141M
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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38Loads and motions of an F-106B flying through thunderstorms
By Roger M. Winebarger
“Loads and motions of an F-106B flying through thunderstorms” Metadata:
- Title: ➤ Loads and motions of an F-106B flying through thunderstorms
- Author: Roger M. Winebarger
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1986
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Loads and motions of an F-106B flying through thunderstorms” Subjects and Themes:
- Subjects: ➤ Aerodynamic forces - Aerodynamic load - Aerodynamic loads - Airplanes - Flight characteristics - Gusts - Pilot performance - Piloting - Storms (Meteorology) - Thunderstorms
Edition Identifiers:
- The Open Library ID: OL16152791M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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39Loads and Aeroelasticity Division research and technology accomplishments for FY 1987 and plans for FY 1988
By S. C. Dixon
“Loads and Aeroelasticity Division research and technology accomplishments for FY 1987 and plans for FY 1988” Metadata:
- Title: ➤ Loads and Aeroelasticity Division research and technology accomplishments for FY 1987 and plans for FY 1988
- Author: S. C. Dixon
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1988
- Publish Location: Hampton, Va - [Springfield, Va
“Loads and Aeroelasticity Division research and technology accomplishments for FY 1987 and plans for FY 1988” Subjects and Themes:
- Subjects: Aerodynamic loads - Aeroelasticity - Research and development - Planning
Edition Identifiers:
- The Open Library ID: OL15418753M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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40Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements
By R. A. DiTaranto
“Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements” Metadata:
- Title: ➤ Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements
- Author: R. A. DiTaranto
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989
- Publish Location: [Springfield, Va - Hampton, Va
“Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements” Subjects and Themes:
- Subjects: ➤ Vibratory loads - Helicopter design - Vibration measurement - Vibration - Aerodynamic loads - Airframes - AH-1G helicopter
Edition Identifiers:
- The Open Library ID: OL16126930M
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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41Active load control during rolling maneuvers
By Jessica A. Woods-Vedeler
“Active load control during rolling maneuvers” Metadata:
- Title: ➤ Active load control during rolling maneuvers
- Author: Jessica A. Woods-Vedeler
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Springfield, VA - Hampton, Va
“Active load control during rolling maneuvers” Subjects and Themes:
- Subjects: ➤ Aerodynamic loads - Control surfaces - Wind tunnel tests - Flexible wings - Active control - Wing loading - Roll
Edition Identifiers:
- The Open Library ID: OL15408536M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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42Final technical report for aeroelastic analysis of counter rotation fans
By Theo G. Keith
“Final technical report for aeroelastic analysis of counter rotation fans” Metadata:
- Title: ➤ Final technical report for aeroelastic analysis of counter rotation fans
- Author: Theo G. Keith
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Final technical report for aeroelastic analysis of counter rotation fans” Subjects and Themes:
- Subjects: ➤ Prop-fan technology - Aerodynamic loads - Turbomachinery - Counter rotation - Dynamic characteristics - Aeroelasticity - Flutter - Fatigue life
Edition Identifiers:
- The Open Library ID: OL18131915M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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43Evaluation of the NASA arc jet capabilities to support mission requirements
By United States. National Aeronautics and Space Administration. Office of the Chief Engineer
“Evaluation of the NASA arc jet capabilities to support mission requirements” Metadata:
- Title: ➤ Evaluation of the NASA arc jet capabilities to support mission requirements
- Author: ➤ United States. National Aeronautics and Space Administration. Office of the Chief Engineer
- Language: English
- Number of Pages: Median: 112
- Publisher: ➤ National Aeronautics and Space Administration, Office of the Chief Engineer
- Publish Date: 2010
- Publish Location: Washington, D.C.]
“Evaluation of the NASA arc jet capabilities to support mission requirements” Subjects and Themes:
- Subjects: ➤ Aerodynamic loads - Aerothermodynamics - Ground tests - Spacecraft design - Test facilities - Thermal protection - Reentry shielding
Edition Identifiers:
- The Open Library ID: OL43879994M
- Online Computer Library Center (OCLC) ID: 755932872
Access and General Info:
- First Year Published: 2010
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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44Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading
By Ellis, John R.
“Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading” Metadata:
- Title: ➤ Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading
- Author: Ellis, John R.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: [Cleveland, Ohio]
“Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading” Subjects and Themes:
- Subjects: ➤ Aerodynamic loads - Aircraft models - Fatigue (Materials) - Loads (Forces) - Materials selection - Stress analysis - Stress cycles - Structural design criteria
Edition Identifiers:
- The Open Library ID: OL16094089M
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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45Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
By Forooz F. Badavi
“Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight” Metadata:
- Title: ➤ Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
- Author: Forooz F. Badavi
- Number of Pages: Median: 51
- Publisher: Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight” Subjects and Themes:
- Subjects: Aerodynamic loads - Helicopters - Rotary wings
Edition Identifiers:
- The Open Library ID: OL18929490M
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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