Performance prediction and optimization for liquid rocket engine nozzle-Reference-Cited by-同舟云学术

Performance prediction and optimization for liquid rocket engine nozzle

Published:2007-03 Issue:2-3 Volume:11 Page:155-162
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cai Guobiao,Fang Jie,Xu Xu,Liu Minghao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference9 articles.

1. G. Candler, J. Perkins, Effects of vibrational nonequilibrium on axisymmetric hypersonic nozzle design, AIAA Paper 91-0297, 1991

2. Influence of chemical kinetics and unmixedness on burning in supersonic hydrogen flames;Evans;AIAA Journal,1980

3. Pressure based calculation procedure for viscous flows at all speeds in arbitrary configurations;Karki;AIAA Journal,1989

4. S. Kim, Calculations of low Reynolds number rocket nozzles, AIAA Paper 93-0888, 1993

5. M.L. Mason, L.E. Putnam, R.J. Re, The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions, NASA-TP-1704, 1980

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