Numerical simulation of scramjet inlet flow fields /

Bibliographic Details

Main Author:	Kumar, Ajay (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, May 1986.
Series:	NASA technical paper ; 2517.
Subjects:	Computational fluid dynamics. Inlet flow. Turbulent flow. Mach number. Three dimensional flow.
Online Access:	https://purl.fdlp.gov/GPO/gpo106416