Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 52
Book Description
An Investigation to Determine the Stability Characteristics of Three Supersonic-impact Ballistic Reentry Shapes at Mach Numbers from 1.2 to 4.2
Author: Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05
Author: Static Stability Investigation of Supersonic-impact Ballistic Reentry Shapes at Mach Numbers of 2.55 and 3.05
Author: John M. SwihartExperimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Number of 1.93, 2.55 and 3.05
Author: Odell A. MorrisAn Exploratory Investigation in a Ballistic Range of the Stability Derivatives of a Simple Airplane Configuration at Low Supersonic Speeds
Author: Charles E. DeRosePublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30
Book Description
Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87
Author: Donald T. GregoryPublisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
Book Description
Scientific and Technical Aerospace Reports
Author: An Analysis of the Stability and Control of Ballistic Supersonic Impact Reentry Bodies
Author: John D. BirdPreliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback
Author: Charles T. D'AiutoloPublisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
Book Description
Author: Robert M. Lust