Three-dimensional unsteady flow simulation of compressed truncated perfect nozzles

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Yonezawa, Koichi ^a   Yokota, Kazuhiko ^b   Tsujimoto, Yoshinobu ^a   Sakazume, Norio ^c   Watanabe, Yasuhide ^c  

^a OSAKA UNIVERSITY   (Japan)

^b NAGOYA INSTITUTE OF TECHNOLOGY   (Japan)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ASYMMETRIC FLOWS; INTERNAL SHOCKS; NOZZLE PRESSURE RATIO; RESTRICTED SHOCK SEPARATION; SUPERSONIC JETS; THREE-DIMENSIONAL NAVIER-STOKES EQUATIONS; THREE-DIMENSIONAL UNSTEADY FLOW; WALL-PRESSURE DISTRIBUTION;

FLOW PATTERNS; NAVIER STOKES EQUATIONS; PROPULSION; SUPERSONIC AERODYNAMICS; THREE DIMENSIONAL; TRANSIENTS;

NOZZLES;

EID: 84896891351     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

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2. Takahashi, M., et al, "Transient Flow Simulation of a Compressed Truncated Perfect Nozzle, " AIAA-2001-3681, 2001.
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10. Frey, M. and Hagemann, G., "Restricted Shock Separation in Rocket Nozzles, " Journal of Propulsion and Power, Vol. 16, No. 3, 2000, pp. 478-484.
11. Frey, M., and Hagemann, G., "Status of Flow Separation Prediction in Rocket Nozzles, " AIAA paper, 98-3619, 1998.