Theoretical prediction of the effects of vortex flows on the loading, forces, and moments of slender aircraft / J. Richard Spahr.
A theoretical method based on slender-body theory is presented for the stepwise calculation of vortex paths in the presence of wing-body combinations and the determination of the load distributions, forces, and moments on the combinations due to the vortices. Comparisons of calculated and experiment...
Saved in:
| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
1961.
|
| Series: | NASA technical report ;
R-101. |
| Subjects: |
Norlin Library - Government Information - US
| Call Number: |
NAS 1.12:101
|
|---|---|
| NAS 1.12:101 | Available Place a Hold |