1-24 of 45 Books
Modal analysis of UH-60A instrumented rotor blades
Modal analysis of UH-60A instrumented rotor blades
By Karen S. Hamade
Development of a low-aspect ratio fin for flight research experiments
Development of a low-aspect ratio fin for flight research experiments
By David M. Richwine
A new higher-order composite theory for analysis and design of high speed tilt-rotor blades
A new higher-order composite theory for analysis and design of high speed tilt-rotor blades
By Thomas R. McCarthy
Finite element thermo-viscoplastic analysis of aerospace structures
Finite element thermo-viscoplastic analysis of aerospace structures
By Ajay K. Pandey
Full-scale hingeless rotor performance and loads
Full-scale hingeless rotor performance and loads
By Randall L. Peterson
Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program
Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program
By J. B. Graham
Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
By David S. Dolling
Aerodynamic interference of high speed ground vehicles
Aerodynamic interference of high speed ground vehicles
By G. W. Johnston
Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
By Ken Gee
Summary of the modeling and test correlations of a NASTRAN finite element vibrations model for the AH-1G helicopter
Summary of the modeling and test correlations of a NASTRAN finite element vibrations model for the AH-1G helicopter
By J. D. Cronkhite
Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
By Bruce Charles
Simultaneous optical measurements of axial and tangential steady-state blade deflections
Simultaneous optical measurements of axial and tangential steady-state blade deflections
By Anatole P Kurkov
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
By Ramadas K. Prabhu
Aircraft loads due to turbulence and their impact on design and certification
Aircraft loads due to turbulence and their impact on design and certification
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Aircraft dynamic loads due to flow separation
Aircraft dynamic loads due to flow separation
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Manual on the flight of flexible aircraft in turbulence
Manual on the flight of flexible aircraft in turbulence
By John C. Houbolt
Surface pressure measurements on the wing of a wind tunnel model during steady rotation
Surface pressure measurements on the wing of a wind tunnel model during steady rotation
By Colin A. Martin
Improvements to the missile aerodynamic prediction code DEMON3
Improvements to the missile aerodynamic prediction code DEMON3
By Marnix F. E. Dillenius
Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
By Forooz F. Badavi
Rotorcraft dynamics 1984
Rotorcraft dynamics 1984
By Specialists' Meeting on Rotorcraft Dynamics (2nd 1984 Ames Research Center)
Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects
Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects
By Martin R. Waszak
A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing
A description of the A.R.A. two-dimensional pitch and heave rig and some results from the NACA 0012 wing
By R. H. Landon
Some aspects of aircraft dynamic loads due to flow separation
Some aspects of aircraft dynamic loads due to flow separation
By D. G. Mabey
Loads and Aeroelasticity Division research and technology accomplishments for FY 1987 and plans for FY 1988
Loads and Aeroelasticity Division research and technology accomplishments for FY 1987 and plans for FY 1988
By S. C. Dixon