Research Catalog

Details

Additional authors

1. NASA Glenn Research Center, issuing body.
2. United States. National Aeronautics and Space Administration, sponsoring body.

Description

1. 1 online resource (16 pages) : color illustrations.

Series statement

1. NASA/TM ; 2014-216634

Uniform title

1. NASA technical memorandum ; 2014-216634.

Subject

1. Computational fluid dynamics
2. Pulse detonation engines
3. Runge-Kutta method
4. Propellant combustion
5. Rotary engines

Call number

1. GPO Internet NAS 1.15:2014-216634

Note

1. Title from title screen (viewed on April 29, 2015).
2. "March 2014."
3. "Prepared for SciTech 2014 sponsored by the American Institute of Aeronautics and Astronautics, National Harbor, Maryland, January 13-17, 2014."

Bibliography (note)

1. Includes bibliographical references (pages 15-16).

Funding (note)

1. Sponsored by the National Aeronautics and Space Administration

Author

1. Paxson, Daniel E., author.

Title

1. Numerical analysis of a rotating detonation engine in the relative reference frame / Daniel E. Paxson.

Publisher

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

Type of content

1. text

Type of medium

1. computer

Type of carrier

1. online resource

Series

1. NASA/TM ; 2014-216634
2. NASA technical memorandum ; 2014-216634.

Bibliography

1. Includes bibliographical references (pages 15-16).

Funding

1. Sponsored by the National Aeronautics and Space Administration [WBS 794072.02.03.05.04]
2. AIAA-2014-0284 [E-18837] [GRC-E-DAA-TN12556]

Connect to:

1. https://purl.fdlp.gov/GPO/gpo57039

Added author

1. NASA Glenn Research Center, issuing body.
2. United States. National Aeronautics and Space Administration, sponsoring body.

Gpo item no.

1. 0830-D (online)

Sudoc no.

1. NAS 1.15:2014-216634