Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design /

Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design /

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Bibliographic Details
Main Author:	Wadel, Mary F. (Author)
Format:	Government Document Electronic eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1998.
Series:	NASA technical memorandum ; 1998-206313.
Subjects:	Rocket engines. Aspect ratio. Combustion chambers. Academic theses.
Online Access:	CONNECT

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