Wind tunnel tests of hypersonic inlets for ramjet modules of ramjet-scramjet combined engine

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 28, Issue 4, 2007, Pages 783-790

  Tan, Hui Jun ^a   Guo, Rong Wei ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Hypersonic inlet; Ramjet; Ramjet scramjet combined engine; Wind tunnel test

Indexed keywords

COMBUSTION; DUCTS; ENTHALPY; FLOW PATTERNS; MACH NUMBER; PRESSURE; RAMJET ENGINES;

HYPERSONIC INLET; MASS FLOW RATIO; RAMJET SCRAMJET COMBINED ENGINE; TOTAL PRESSURE RECOVERY COEFFICIENT;

WIND TUNNELS;

EID: 34547996101     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

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