Research Catalog

Title

Perormance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydorgen-oxygen rocket [microform] / Lynn A. Arrington and Brian D. Reed.

Author

Arrington, Lynn A.

Publication

[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]

Details

Additional Authors

• Reed, Brian D.
• Lewis Research Center.

Description

20 p. : ill.

Series Statement

NASA technical memorandum ; 105967

Uniform Title

NASA technical memorandum ; 105967.

Subject

• Axisymmetric flow
• Coolants
• Film cooling
• Fluid injection
• Hydrogen
• Hydrogen oxygen engines
• Propulsion system performance
• Reacting flow
• Three dimensional flow

Bibliography (note)

• Includes bibliographical references (p. 8-9).

Reproduction (note)

• Microfiche.

Call Number

GPO Microfiche NAS 1.15:105967

OCLC

marcive658186223

Author

Arrington, Lynn A.

Title

Perormance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydorgen-oxygen rocket [microform] / Lynn A. Arrington and Brian D. Reed.

Imprint

[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]

Series

NASA technical memorandum ; 105967

NASA technical memorandum ; 105967.

Bibliography

Includes bibliographical references (p. 8-9).

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993]. 1 microfiche.

Added Author

Reed, Brian D.

Lewis Research Center.

Other Form:

Online version: Arrington, Lynn A. Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen-oxygen rocket. (OCoLC)658189070

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:105967