Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds /

Bibliographic Details

Main Author:	Kim, Hyun D.
Corporate Author:	NASA Glenn Research Center
Other Authors:	Frate, Franco C.
Format:	Government Document Book
Language:	English
Published:	[Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2001]
Series:	NASA technical memorandum ; 201565.
Subjects:	Aerodynamic characteristics. Angle of attack. COMPUTATIONAL FLUID DYNAMICS. Dimensional analysis. BOUNDARY LAYER TRANSITION. Flow distribution.
Online Access:	Adobe Acrobat Reader required