Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage /
by Samuel M. Dollyhigh.
Description
| Main Author: | Dollyhigh, Samuel M. |
|---|---|
| Language(s): | English |
| Published: |
Washington, D.C. : National Aeronautics and Space Administration ; 1974. |
| Subjects: |
Fighter planes.
Camber (Aerofoils) Stability of airplanes, Longitudinal. |
| Note: |
Prepared at Langley Research Center. Cover title. |
| Physical Description: |
96 p. :
chiefly ill. ;
27 cm.
|
| Locate a Print Version: |
Find in a library |
Viewability
| Item Link | Original Source |
|---|---|
| Full view | University of Illinois at Urbana-Champaign |