In this paper, viscous effects on hypersonic vehicle are investigated. Firstly, viscous aerodynamic is modeled based on reference temperature method, and viscous aerodynamic lift, drag and pitching moment are calculated by the model. And then, aerodynamic forces and elastic deformation are analyzed by comparing with viscous effects on/off. In final, considering the thermal choking condition, longitudinal velocity and attitude boundary values are discussed.
Simulation Analysis of Viscous Effects on Dynamic Performance of Hypersonic Vehicle
Applied Mechanics and Materials ; 433-435 ; 1979-1983
2013-10-15
5 pages
Article (Journal)
Electronic Resource
English
Viscous Effects for a Hypersonic Vehicle Model
AIAA | 2008
|Viscous Effects for a Hypersonic Vehicle Model
British Library Conference Proceedings | 2008
|