Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow /
Saved in:
| Main Author: | |
|---|---|
| Format: | Government Document Electronic eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
December 1968.
|
| Series: | NASA technical note ;
D-4929. |
| Subjects: | |
| Online Access: | CONNECT |
