Cover image for Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63
Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63
Title:
Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63
Author:
Miller, Davis S.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration, 1971.
Physical Description:
30 pages : illustrations ; 27 cm.
General Note:
Prepared at Langley Research Center.

"N71-23125."
Language:
English
Format :
Book