Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach number 0.2
Title:
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach number 0.2
Author:
Penland, Jim A.
Personal Author:
Publication Information:
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Physical Description:
80 pages : illustrations ; 27 cm.
General Note:
Issued Sept. 1978.
Language:
English
Format :
Book