Investigation of flow in isolator of hypersonic inlet

Tuijin Jishu/Journal of Propulsion Technology

Volumn 23, Issue 4, 2002, Pages 311-314

  Zhang, Kun Yuan ^a   Wang, Cheng Peng ^a   Yang, Jian Jun ^a   Xu, Jing Lei ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Flow characteristic; Hypersonic combustion; Inlet; Inlet flow; Isolator; Ramjet engine; Wind tunnel test

Indexed keywords

INTAKE SYSTEMS; WIND TUNNELS;

FLOW CHARACTERISTIC; HYPERSONIC COMBUSTION; INLET; INLET FLOW; ISOLATOR;

RAMJET ENGINES;

EID: 0036700175     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. Pratt D T, Heiser W H. Isolator-combustor interaction in a dual-mode scramjet engine [R]. AIAA 93-0358.
2. Waltrup P J, Billig F S. Structure of shock waves in cylindrical ducts [R]. J. of AIAA, 1973, 11(10).
3. Jensen J Braendlein B. Review of the marquardl dual mode mach 8 scramjet development [R]. AIAA 96-3037.
4. Fernandez R. RBCC engine technology development-sub-scale inlet experimental results [R]. AIAA 97-0612.