1-17 of 17 Books
1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
By NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)
Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
By Dale R. Satran
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
By Daniel W. Banks
Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
By Long P. Yip
Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
By Matthew Robert Whiting
HiMAT flight program
HiMAT flight program
By Dwain A. Deets
Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
By Christopher A. Lee
Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
By Jerry M. Allen
Visualisation in water of vortex flow over sharp-edged canard configurations
Visualisation in water of vortex flow over sharp-edged canard configurations
By D. H. Thompson
Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization
Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization
By Harry W. Carlson
A computer module used to calculate the horizontal control surface size of a conceputal aircraft design
A computer module used to calculate the horizontal control surface size of a conceputal aircraft design
By Doral R. Sandlin
Space shuttle orbiter trimmed center-of-gravity extension study
Space shuttle orbiter trimmed center-of-gravity extension study
By William I. Scallion
Numerical study of steady and unsteady canard-wing-body aerodynamics
Numerical study of steady and unsteady canard-wing-body aerodynamics
By Eugene L. Tu
Parametric study of a canard-configured transport using conceptual design optimization
Parametric study of a canard-configured transport using conceptual design optimization
By P. Douglas Arbuckle
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
By Ira J. Walker
Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
By Joanne L. Walsh
A theoretical study of the aerodynamic characteristics of low-speed multi-wing aircraft
A theoretical study of the aerodynamic characteristics of low-speed multi-wing aircraft
By Bernard Gagnon