2 options
Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel / Donald A. Durston [and thirteen others].
- Format:
- Book
- Government document
- Author/Creator:
- Durston, D. A., author.
- Series:
- NASA technical publication ; 2018-219879.
- NASA/TP ; 2018-219879
- Language:
- English
- Genre:
- technical reports.
- Technical reports
- Technical reports.
- Physical Description:
- 1 online resource (xxvi, 489 pages) : color illustrations.
- Other Title:
- Nozzle plume/shock interaction experimental and computational sonic boom analyses from the National Aeronautics and Space Administration Ames 9-by 7-foot supersonic wind tunnel
- Place of Publication:
- Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, December 2018.
- Notes:
- "December 2018."
- Includes bibliographical references (pages 238-240).
- Description based on online resource, PDF version; title from title page (NASA, viewed June 5, 2019).
- OCLC:
- 1103608584
The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.