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].
- Author
- Durston, D. A.
- Additional Titles
- 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
- Published
- Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, December 2018.
- Physical Description
- 1 online resource (xxvi, 489 pages) : color illustrations
- Additional Creators
- Ames Research Center
Access Online
- Series
- Restrictions on Access
- Free-to-read Unrestricted online access
- Report Numbers
- NAS 1.60:2018-219879
- Subject(s)
- Note
- "December 2018."
- Bibliography Note
- Includes bibliographical references (pages 238-240).
- Action Note
- committed to retain. Federal Depository Library Program (FDLP). For information on our retention commitment, please contact Microforms and Government Information.
View MARC record | catkey: 27405383