1-24 of 76 Books
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By R. A. Piziali
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
By Wendy B. Lessard
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By Robert S. Jankovsky
F-18 High Alpha Research Vehicle surface pressures
F-18 High Alpha Research Vehicle surface pressures
By David F. Fisher
Rocket-based combined cycle engine technology development
Rocket-based combined cycle engine technology development
By J. R. DeBonis
Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction
Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction
By John R. Micol
Measurements of unsteady pressure and structural response for an elastic supercritical wing
Measurements of unsteady pressure and structural response for an elastic supercritical wing
By Clinton V. Eckstrom
Analysis of two-phase flow in damper seals for cryogenic turbomachinery
Analysis of two-phase flow in damper seals for cryogenic turbomachinery
By Grigory L. Arauz
Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
By Thomas C. Corke
Laser scanning system for pressure and temperature paints
Laser scanning system for pressure and temperature paints
By John Sullivan
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By William G. Johnson
Computer code study of asteroid entry into Venusian atmosphere
Computer code study of asteroid entry into Venusian atmosphere
By Robert M. Schmidt
Atmospheric probe model
Atmospheric probe model
By Jerald M. Vogel
Experimental aerothermodynamic research of hypersonic aircraft
Experimental aerothermodynamic research of hypersonic aircraft
By Joseph W. Cleary
Evaluation of 3D inverse code using rotor 67 as test case
Evaluation of 3D inverse code using rotor 67 as test case
By T. Dang
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
By Sheryll Goecke Powers
Wing pressure distributions from subsonic tests of a high-wing transport model
Wing pressure distributions from subsonic tests of a high-wing transport model
By Zachary T. Applin
Effects of winglets on a first-generation jet transport wing
Effects of winglets on a first-generation jet transport wing
By Robert R. Meyer
Solar rocket plume/mirror interactions
Solar rocket plume/mirror interactions
By Sheng-Tao Yu
Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
By Zachary T. Applin
Calculation of multistage turbomachinery using steady characteristic boundary conditions
Calculation of multistage turbomachinery using steady characteristic boundary conditions
By Rodrick V. Chima
Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
By David F. Fisher
Vibroacoustic response of pad structures to space shuttle launch acoustic loads
Vibroacoustic response of pad structures to space shuttle launch acoustic loads
By R. N. Margasahayam
Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
By Dale Ashby