Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions
Title:
Effect of subsonic inlet lip geometry on predicted surface and flow Mach number distributions
Author:
Albers, James A.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1973.
Physical Description:
35 pages : illustrations ; 27 cm.
General Note:
Cover title.
Prepared at Lewis Research Center.
Language:
English
Added Author:
Added Corporate Author:
Format :
Book