Research Catalog

Title

Impact of an exhaust throat on semi-idealized rotating detonation engine performance / Daniel E. Paxson.

Author

Paxson, Daniel E.

Publication

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2016.

Details

Additional Authors

NASA Glenn Research Center, issuing body.

Description

1 online resource (12 pages) : color illustrations.

Series Statement

NASA/TM ; 2016-219076

Uniform Title

NASA technical memorandum ; 2016-219076.

Subjects

• Propulsion system performance
• Inviscid flow
• Fuel flow
• Exhaust flow simulation
• Computational fluid dynamics

Note

• Title from title screen (viewed on June 8, 2016).
• "April 2016."
• "Prepared for the Scitech 2016 sponsored by the American Institute of Aeronautics and Astronautics, San Diego, California, January 4-8, 2016."
• "AIAA-2016-11647."

Bibliography (note)

• Includes bibliographical references (pages 11-12).

Call Number

GPO Internet NAS 1.15:2016-219076

OCLC

marcive951418247

Author

Paxson, Daniel E., author.

Title

Impact of an exhaust throat on semi-idealized rotating detonation engine performance / Daniel E. Paxson.

Publisher

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2016.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2016-219076

NASA technical memorandum ; 2016-219076.

Bibliography

Includes bibliographical references (pages 11-12).

Connect to:

https://purl.fdlp.gov/GPO/gpo68694

Added Author

NASA Glenn Research Center, issuing body.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2016-219076