Plume and divert jet effects on missile flowfields at higher altitudes

AIAA Paper

Volumn , Issue , 2004, Pages 6913-6925

  Papp, J L ^a   Yellin, K A ^a   Dash, S M ^a  

^a Syst Simulation Dvmt Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; JETS; MATHEMATICAL MODELS; MONTE CARLO METHODS; PARALLEL PROCESSING SYSTEMS; PARAMETER ESTIMATION; THERMAL PLUMES; TURBULENCE; VELOCITY MEASUREMENT;

DIRECT SIMULATION MONTE CARLO (DSMC); DIVERT JET EFFECTS; GRID DYNAMICS; MISSILE FLOWFIELDS;

MISSILES;

EID: 2942746671     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1110     Document Type: Conference Paper

References (12)

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2. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 8-11, 2001.
3. http://icb.nasa.gov/swoy2002/
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7. Glass C.E., Numerical Study of Rarefied Hypersonic Flow Interacting With A Continuum Jet. Doctoral Dissertation, Pennsylvania State University, August 1999.
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10. Staack, D., McDaniel, J.C., Glass, C.E., and Miller C., "Experimental Study of Interacting Rarefied and Continuum Flows" AIAA Paper 2001-2762, 2001.
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