Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel /

Bibliographic Details

Main Author:	Chima, Rodrick V.
Corporate Authors:	NASA Glenn Research Center, AIAA Applied Aerodynamics Conference
Other Authors:	Hirt, Stefanie M., Reger, Robert
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2011]
Series:	NASA technical memorandum ; 2011-217224.
Subjects:	Supersonic inlets. Computational fluid dynamics. Mass flow. Flight paths. Supersonic aircraft. Stability.
Online Access:	https://purl.fdlp.gov/GPO/gpo21441