Detached eddy simulation of a generic scramjet inlet and combustor

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Peterson, David M ^a,b   Candler, Graham V ^a,b   Drayna, Travis W ^a,c  

^a UNIVERSITY OF MINNESOTA   (United States)

^b Department of Aerospace Engineering and Mechanics ^*

^c GoHypersonic Inc

Author keywords

[No Author keywords available]

Indexed keywords

ADDITIONAL COSTS; AUTOMATED GENERATION; BEZIER CURVE; CHEMICAL SOURCES; CURRENT SIMULATION; DETACHED EDDY SIMULATIONS; ENERGY-CONSERVING; FINITE-RATE CHEMISTRY; HIGH QUALITY; IMPLICIT TIME INTEGRATION; MODELING APPROACH; NUMERICAL SCHEME; REYNOLDS-AVERAGED NAVIER-STOKES; SCRAMJET ENGINES; SCRAMJET INLETS; SUBGRID MODEL; TIME-SCALES; TURBULENCE CLOSURES;

AEROSPACE ENGINEERING; ATMOSPHERIC BOUNDARY LAYER; COMBUSTION; COMBUSTORS; FLUORINE; HYDROGEN; HYPERSONIC INLETS; LARGE EDDY SIMULATION; NAVIER STOKES EQUATIONS; OPTIMIZATION; TURBULENCE; TURBULENT FLOW;

COMPUTER SIMULATION;

EID: 78549279128     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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