Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry /

Bibliographic Details

Main Author:	Herring, Gregory C.
Corporate Author:	Langley Research Center
Other Authors:	Meyers, James F.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Series:	NASA technical memorandum ; 217052.
Subjects:	Velocity measurement. Sonic booms. Flow characteristics. Supersonic speed. Oblique shock waves.
Online Access:	https://purl.fdlp.gov/GPO/gpo13301