Evaluation of aero-propulsive performance for integrated hypersonic vehicle

Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics

Volumn 21, Issue 2, 2007, Pages 63-67

  He, Yuan Yuan ^a   Ni, Hong Li ^a   Le, Jia Ling ^a  

^a CHINA AERODYNAMICS RESEARCH AND DEVELOPMENT CENTER   (China)

Author keywords

Aero propulsive performance; CFD; Computational errors; Experimental data; Integrated hypersonic vehicle

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLOW FIELDS; FLUID STRUCTURE INTERACTION; HYPERSONIC FLOW; PROPULSION; VEHICLES; WIND TUNNELS;

AERO PROPULSIVE PERFORMANCE; COMPUTATIONAL ERRORS; EXPERIMENTAL DATA; INTEGRATED HYPERSONIC VEHICLE;

AIRFRAMES;

EID: 34547359148     PISSN: 16729897     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (4)

1. ABDELKADER Frendi. On the CFD support for the Hyper-X aerodynamic database[R]. AIAA 99-0885.
2. CHARLES E Cockrell, et al. Integrated aero-propulsive CFD methodology for the Hyper-X flight experiment[R]. AIAA 2000-4010.
3. WALTER C Engelund, et al. Propulsion system airframe integration issues and aerodynamic database development for the Hyper-X flight research vehicle[R]. ISOABE 99-7215.