Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6
Title:
Effects of leading-edge sweep angle and design lift coefficient on performance of a modified arrow wing at a design Mach number of 2.6
Author:
Mack, Robert J.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1974.
Physical Description:
49 pages : illustrations ; 27 cm.
General Note:
Cover title.
Prepared at Langley Research Center.
Language:
English
Added Corporate Author:
Format :
Book