Assessment of synthetic inflow generation for simulating injection into a supersonic crossflow

A Collection of Technical Papers - 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 3, Issue , 2006, Pages 2195-2208

  Peterson, David M ^a,b,c   Subbareddy, Prarnod K ^a,b,c   Candler, Graham V ^a,b,c  

^a UNIVERSITY OF MINNESOTA   (United States)

^b University of Minnesota   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EDDY SIMULATION; MOLE FRACTIONS; SUPERSONIC CROSSFLOW; SYNTHETIC INFLOW GENERATION;

BOUNDARY LAYER FLOW; COMPUTER SIMULATION; EDDY CURRENTS; KINETIC ENERGY; SUPERSONIC AERODYNAMICS; TIME VARYING CONTROL SYSTEMS;

SUPERSONIC FLOW;

EID: 33947267518     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

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