Problems of numerical diffusion found in scramjets

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 1, Issue , 2005, Pages 111-121

  Kouchi, Toshinori ^a,c   Mitani, Tohru ^a,c   Masuya, Goro ^b,d  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOHOKU UNIVERSITY   (Japan)

^c Kakuda Space Propulsion Center   (Japan)

^d Department of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; COMPUTER SIMULATION; CONVERGENCE OF NUMERICAL METHODS; SUPERSONIC AERODYNAMICS; VISCOSITY;

CIRCULAR HOLE; NUMERICAL DIFFUSION; SCRAMJET COMBUSTOR;

COMBUSTORS;

EID: 29044434566     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3216     Document Type: Conference Paper

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