Scramjet inlet flow computations by hybrid grid method

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Kodera, Masatoshi ^a   Nakahashi, Kazuhiro ^a   Hiraiwa, Tetsuo ^b,c   Kanda, Takeshi ^b,c   Mitani, Tohru ^b,d  

^a TOHOKU UNIVERSITY   (Japan)

^b KAKUDA RESEARCH CENTER   (Japan)

^c Ramjet Propulsion Research Division

^d Ramjet Combustion Laboratory

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTION; ENGINES; FLOW FIELDS; MACH NUMBER; NUMERICAL METHODS; RAMJET ENGINES; STRUTS; TURBULENCE MODELS;

CELL-VERTEX SCHEMES; COMPUTATIONAL RESULTS; COMPUTATIONAL TIME; HIGH-SPEED PROPULSIONS; IMPLICIT TIME INTEGRATION; INFLOW MACH NUMBER; LOW VELOCITY REGION; UNSTRUCTURED HYBRID GRIDS;

NAVIER STOKES EQUATIONS;

EID: 84983171139     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-962     Document Type: Conference Paper

References (16)

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