| 90 |
 Subsonic lift-dependent drag due to the trailing vortex wake for wings without camber or twist. |
74035 |
| 90 |
Subsonic lift-dependent drag due to boundary layer of plane, symmetrical section wings.
|
66032 |
| 90 |
Introductory sheet on subcritical lift-dependent drag of wings. |
66031 |
| 90 |
Pitching moment of low-aspect-ratio cropped-delta wings up to high angles of attack at subsonic speeds. |
95022 |
| 90 |
Computer program for estimation of spanwise loading of wings with camber and twist in subsonic attached flow. Lifting-surface theory. (With Appendix A: effect of plain flaps.) |
95010 |
| 90 |
Normal force of low-aspect-ratio cropped-delta wings up to high angles of attack at subsonic speeds. |
93034 |
| 90 |
Program for calculation of maximum lift coefficient of plain aerofoils and wings at subsonic speeds. |
93015 |
| 90 |
Normal force and pitching moment of low aspect ratio cropped-delta wings up to high angles of attack at supersonic speeds. |
90013 |
| 90 |
The maximum lift coefficient of plain wings at subsonic speeds. |
89034 |
| 90 |
Method for the rapid estimation of spanwise loading of wings with camber and twist in subsonic attached flow. |
83040 |
