Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0
Title:
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0
Author:
Penland, Jim A.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1979.
Physical Description:
145 unnumbered pages : illustrations ; 27 cm.
General Note:
"Langley Research Center."
"December 1979"--Cover.
Language:
English
Subject Term:
Added Author:
Format :
Book