Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds /
Jack Nugent, Odis C. Pendergraft, Jr.
Description
- Language(s)
-
English
- Published
-
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1987.
- Note
-
Prepared at Ames Research Center.
"March 1987"--Cover.
- Physical Description
-
120 p. :
ill. ;
28 cm.
Viewability
Item Link |
Original Source |
Full view
|
University of Illinois at Urbana-Champaign
|