Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations /
Samuel M. Dollyhigh.
Description
| Main Author: | Dollyhigh, Samuel M. |
|---|---|
| Language(s): | English |
| Published: |
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1979. |
| Subjects: |
Fighter planes
>
Fighter planes /
Design and construction.
Supersonic wind tunnels. Aerodynamics, Supersonic. |
| Note: |
Feb. 1979. "Langley Research Center, Hampton, Virginia." |
| Physical Description: |
187 p. :
ill. ;
27 cm.
|
| Locate a Print Version: |
Find in a library |
Viewability
| Item Link | Original Source |
|---|---|
| Full view | University of Illinois at Urbana-Champaign |