Numerical study on a thermal response of the jet vane system in a rocket nozzle

AIAA Paper

Volumn , Issue , 2004, Pages 12341-12348

  Yu, M S ^a   Lee, J W ^a   Cho, H H ^a,c   Hwang, K Y ^b   Bae, J C ^b  

^a Yonsei University   (South Korea)

^b Agency for Defence Development   (South Korea)

^c Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTATION THEORY; FINITE DIFFERENCE METHOD; INTEGRAL EQUATIONS; JETS; NOZZLES; PROBLEM SOLVING;

GRID POINTS; THERMAL BOUNDARY CONDITIONS; THRUST VECTOR CONTROL;

ROCKET ENGINES;

EID: 2942720694     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. R. P. Roger, S. C. Chan and J. D. Hundrey, "CFD Analysis for the Lift and Drag on a Fin/Mount as a Jet Vane TVC for Boost Control," AIAA Paper 95-0083.
2. Gubertov, A., Development of the JV system, Keldysh Research Center, 2000.
3. rd Edition, McGraw-Hill Inc., 1993.
4. Patrick, H. O. and William, E. C., Compressible Fluid Flow International Editions, McGraw-Hill Inc., 1997.