The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios [microform] / Kenneth J. Kacynski and Joe D. Hoffman.

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Bibliographic Details
Main Author:	Kacynski, Kenneth J.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Hoffman, Joe D., 1934-
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], [1994]
Series:	NASA technical memorandum ; 106617.
Subjects:	Heat > Transmission. Thermal diffusivity. Film cooling. Flow distribution. Heat transfer. Hydrogen oxygen engines. Nozzle flow. Sweat cooling. Thermal diffusion.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:106617
NAS 1.15:106617	Restricted Place a Hold