Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket /

Bibliographic Details

Main Author:	Arrington, Lynn A.
Corporate Author:	Lewis Research Center
Other Authors:	Reed, Brian D.
Format:	Government Document eBook
Language:	English
Published:	[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]
Series:	NASA technical memorandum ; 105967.
Subjects:	Axisymmetric flow. Coolants. Film cooling. Fluid injection. Hydrogen. Hydrogen oxygen engines. Propulsion system performance. Reacting flow. Three dimensional flow.
Online Access:	https://purl.fdlp.gov/GPO/LPS125649