Structure of a supersonic three-dimensional cylinder/offset-flare turbulent interaction

Journal of Spacecraft and Rockets

Volumn 34, Issue 3, 1997, Pages 294-302

  Gaitonde, Datta ^a,c   Shang, J S ^a,c   Edwards, J R ^b,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b NORTH CAROLINA STATE UNIVERSITY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; COMPRESSIBLE FLOW; COMPUTER SIMULATION; CYLINDERS (SHAPES); DATA REDUCTION; DATABASE SYSTEMS; FLOW INTERACTIONS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; SHOCK WAVES; TOPOLOGY; TURBULENT FLOW;

MACH NUMBER; TURBULENT STRESS; VISCOUS STRESS;

SUPERSONIC AERODYNAMICS;

EID: 0031140862     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3232     Document Type: Article

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