The Hypersonic Arbitrary-Body Aerodynamics (HABA) computer program predicts static and dynamic aerodynamic derivatives at hypersonic speeds for any vehicle geometry. It is intended to be used during conceptual design studies where fast computational speed is required. It uses the same geometry and hypersonic aerodynamic methods as the Mark IV Supersonic/Hypersonic Arbitrary-Body Program (SHABP) developed under sponsorship of the Air Force Flight Dynamics Laboratory; however, the input and output formats have been improved to make it easier to use. This program is available as part of the Department 9140 CAE software.
Hypersonic Arbitrary-Body Aerodynamics (HABA) for conceptual design
1990
103 pages
Report
Keine Angabe
Englisch
Mathematical Sciences , Air Transportation , Energy Use, Supply, & Demand , Manned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Aerodynamics , Hypersonic Flow , A Codes , Reynolds Number , Hypersonic aircraft , Aerodynamic configurations , Computational fluid dynamics , EDB/320201 , EDB/990200
ANALYTIC HYPERSONIC AERODYNAMICS FOR CONCEPTUAL DESIGN OF ENTRY VEHICLES
British Library Conference Proceedings | 2010
|Engineering Index Backfile | 1959
|Rapid Supersonic/Hypersonic Aerodynamics Analysis Model for Arbitrary Geometries
Online Contents | 2017
|Rapid Supersonic/Hypersonic Aerodynamics Analysis Model for Arbitrary Geometries
Online Contents | 2016
|