Characteristics of shock train in two dimensional bends with constant area

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 27, Issue 6, 2006, Pages 1039-1045

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

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Bend duct; Inlet; Isolator; Ramjet; Scramjet; Shock train

Indexed keywords

BOUNDARY LAYERS; CALCULATIONS; COMPUTATIONAL FLUID DYNAMICS; DUCTS; FLOW PATTERNS; INTAKE SYSTEMS; NAVIER STOKES EQUATIONS; PIPELINE BENDS; PRESSURE; RAMJET ENGINES; TWO DIMENSIONAL;

BEND DUCT; INLET; ISOLATOR; MACH NUMBER; SCRAMJET; SHOCK TRAIN;

SHOCK WAVES;

EID: 33846846456     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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