Experimental investigation of a Mach 6 fixed-geometry inlet featuring a swept external-internal compression flow field
Title:
Experimental investigation of a Mach 6 fixed-geometry inlet featuring a swept external-internal compression flow field
Author:
Torrence, Marvin G.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1975.
Physical Description:
61 pages : illustrations ; 27 cm.
General Note:
Cover title.
Prepared at Langley Research Center.
Language:
English
Added Corporate Author:
Format :
Book