http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel
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
1 online resource (xxvi, 489 pages) : color illustrations.
Donald A. Durston [and thirteen others].
Includes bibliographical references (pages 238-240).
NASA technical publication ; 2018-219879