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
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
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
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
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
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
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
Space shuttle orbiter trimmed center-of-gravity extension study
Space shuttle orbiter trimmed center-of-gravity extension study
By William I. Scallion
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
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
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