Effect of sweep on cavity flow fields at subsonic and transonic speeds /

Bibliographic Details

Corporate Author:	Langley Research Center
Other Authors:	Tracy, Maureen B.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Series:	NASA technical memorandum ; 2012-217577.
Subjects:	Cavity flow. Cavities. Flow distribution. Leading edge sweep. Pressure distribution. Sweep angle. Trailing edges. Static pressure.
Online Access:	https://purl.fdlp.gov/GPO/gpo30610