Please use this identifier to cite or link to this item: http://hdl.handle.net/2440/30466
Type: Book chapter
Title: Fundamentals of supercritical mixing and combustion of cryogenic propellants
Author: Smith, J. J.
Citation: Liquid rocket thrust chambers: Aspects of modeling, analysis, and design - Volume 200 - Progress in Astronautics and aeronautics. pp.339-367
Publisher: American Institute of Aeronautics and Astronautics, Inc.
Issue Date: 2004
ISBN: 1563472236
School/Discipline: School of Mechanical Engineering
RMID: 0020042256
Appears in Collections:Mechanical Engineering publications

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