An analysis of the chemically reacting boundary layer during hybrid combustion

Author:

KRIER H.1,KERZNER H.2

Affiliation:

1. Illinois, University, Urbana, Ill.

2. Thiokol Chemical Co., Brigham City, Utah

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. Chung, 1'. bl, "Clieinj.cally Rcacti-ng Non-liquilihriuin Eoundary Layers ,11Advances in Heat 'TPRIISferVol.2, Academic Prcss, London, pp.110-278-7-ihT

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Rotational and Quasiviscous Cold Flow Models for Axisymmetric Hybrid Propellant Chambers;Journal of Fluids Engineering;2010-10-01

2. Hybrid Rocket Fuel Regression Rate Data and Modeling;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

3. Inviscid Models of the Classic Hybrid Rocket;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

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