1-13 of 13 Books
Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements
Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements
By Milton Lamb
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
By Laurence D. Leavitt
NASA/FAA Tailplane Icing Program overview
NASA/FAA Tailplane Icing Program overview
By Thomas P. Ratvasky
A low-speed wind-tunnel investigation of the tailplane effectiveness of a model representing the airbus type of aircraft
A low-speed wind-tunnel investigation of the tailplane effectiveness of a model representing the airbus type of aircraft
By D. A. Lovell
An investigation of the rolling moments due to side-slip on high tailplanes
An investigation of the rolling moments due to side-slip on high tailplanes
By Dennis G. Mabey
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
By Laurence D. Leavitt
Development of a reduced area horizontal tail for a wide body jet aircraft
Development of a reduced area horizontal tail for a wide body jet aircraft
By Jerry J. Rising
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
By Laurence D. Leavitt
Prediction of light aircraft horizontal tail onset flows
Prediction of light aircraft horizontal tail onset flows
By Delbert C. Summey
Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow
Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow
By Osama A. Kandil
Application of linear quadratic control in reduction of aerodynamic forces on aircraft
Application of linear quadratic control in reduction of aerodynamic forces on aircraft
By Shou Yuan Wei
Computation and validation of fluid/structure twin tail buffet response
Computation and validation of fluid/structure twin tail buffet response
By Osama A. Kandil