Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 1.50 to 2.86
Title:
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 1.50 to 2.86
Author:
Penland, Jim A.
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:
81 pages : illustrations ; 27 cm.
General Note:
Prepared at Langley Research Center.
Language:
English
Added Corporate Author:
Format :
Book