Numerical investigation of supersonic flows around a spiked blunt body

Journal of Spacecraft and Rockets

Volumn 32, Issue 1, 1995, Pages 32-42

  Yamauchi, Masafumi ^a,c   Fujii, Kozo ^b,c   Higashino, Fumio ^a,c  

^a TOKYO UNIVERSITY OF AGRICULTURE AND TECHNOLOGY   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Department of Mechanical Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; ANGLE MEASUREMENT; COMPUTATIONAL METHODS; COMPUTER SIMULATION; DRAG; HEAT FLUX; NAVIER STOKES EQUATIONS; PRESSURE MEASUREMENT; SHOCK WAVES; SUPERSONIC FLOW;

HIGH RESOLUTION UPWIND SCHEME; LU ADI TIME INTEGRATION ALGORITHM; MACH NUMBER; SPIKED BLUNT BODY;

SUPERSONIC AERODYNAMICS;

EID: 0029197324     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.26571     Document Type: Article

References (11)

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10. Obayashi, S., Matsushima, K., Fujii, K., and Kuwahara, K., “Improvement in Efficiency and Reliability for Navier-Stokes Computations Using the LU-ADI Factorization Algorithm,” AIAA Paper 86-0338, Jan 1986.
11. Guenther, R. A., and Reding, J. P, “Fluctuation Pressure Environment of a Drag Reduction Spike,” Journal of Spacecraft and Rockets, Vol. 14, No. 12, 1977, pp. 705-710.