Numerical Study and Performance Prediction for Gasgeous Hydrogen/Oxygen Bell Nozzle

Author:

Tsuboi Nobuyuki,Ito Takashi,Miyajima Hiroshi

Publisher

Japan Society for Aeronautical and Space Sciences

Reference28 articles.

1. 1) Gorden, S. and McBride, J. B.: Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman-Jouguet Detonations, NASA SP-273, 1971.

2. 2) 中橋和博,宮島博,木皿且人,毛呂明夫:ロケットノズルの性能予測計算法,航空宇宙技術研究所報告,NAL TR-771,1983.

3. Unified Navier-Stokes flowfield and performance analysis of liquid rocket engines

4. Hot-gas-side and coolant-side heat transfer in liquid rocket engine combustors

5. 5) Wang, T. S.: Multidimentional Unstructured-Grid Liquid Rocket Engine Nozzle Performance and Heat Transfer Analysis, AIAA Paper 2004-4016, 2004.

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1. Numerical Investigations of the Film Cooling Effect on Sub-Scale Rocket Engine Performance;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2008

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