DSMC computations for regions of shock/shock and shock/boundary layer

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Moss, James X ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXISYMMETRIC CONFIGURATIONS; DIRECT SIMULATION MONTE CARLO METHOD; DOUBLE CONES; FLOW CONDITION; GRID RESOLUTION; HOLLOW CYLINDERS; INFORMATION CONCERNING; RESEARCH CENTER;

COMPUTER SIMULATION; CYLINDER CONFIGURATIONS;

AEROSPACE ENGINEERING;

EID: 84897850729     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (30)

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9. Holderi, M. and Harvey, J. Experimental Measurements over Cone/Cone and Cylinder Flare Configurations in Laminar Hypervelocity Flows. AIAA Paper 2001-1031, Jan. 2001.
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30. Bird, G. A.: private communication. Aug. 2000