Research Catalog

Title

Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / Zhuohui J. He [and four others].

Author

He, Zhuohui J.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.

Details

Additional Authors

• NASA Glenn Research Center, issuing body.
• Fundamental Aeronautics Program (U.S.), sponsoring body.

Description

1 online resource (7 pages) : color illustrations.

Series Statement

NASA/TM ; 2014-218117

Uniform Title

NASA technical memorandum ; 2014-218117.

Subject

• Combustion chambers
• Inlet pressure
• Inlet temperature
• Fuel injection
• Combustion temperature
• Nitrogen oxides

Note

• Title from title screen (viewed on March 25, 2015).
• "April 2014."
• "Prepared for the 8th U.S. National Combustion Meeting sponsored by the Western State Section, Combustion Institute, Park City, Utah, May 19-22, 2013."

Bibliography (note)

• Includes bibliographical references (page 7).

Funding (note)

• Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center

Call Number

GPO Internet NAS 1.15:2014-218117

OCLC

marcive905620862

Author

He, Zhuohui J., author.

Title

Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector / Zhuohui J. He [and four others].

Publisher

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2014-218117

NASA technical memorandum ; 2014-218117.

Bibliography

Includes bibliographical references (page 7).

Funding

Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 794072.02.03.05.02

E-18859

Connect to:

https://purl.fdlp.gov/GPO/gpo54279

Added Author

NASA Glenn Research Center, issuing body.

Fundamental Aeronautics Program (U.S.), sponsoring body.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2014-218117