Some divergence characteristics of low-aspect-ratio wings at transonic and supersonic speeds /
The problem of chordwise, or camber, divergence at transonic and supersonic speeds is treated with primary emphasis on slender delta wings having a cantilever support at the trailing edge. Experimental and analytical results are presented for four wing models having apex half-angles of 5 deg, 10 deg...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce,
[1960]
|
| Series: | NASA technical note ;
D-461 |
| Subjects: | |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|