Wake-vortex structure from lift and torque induced on a following wing
- 6 July 1993
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Estimate of loads during wing-vortex interactions by Munk's transverse-flow methodJournal of Aircraft, 1990
- Effect of Wing Fins on Lift-Generated WakesJournal of Aircraft, 1978
- Experimental Study of the Effect of Span Loading on Aircraft WakesJournal of Aircraft, 1976
- Prediction of Span Loading from Measured Wake-Vortex Structure -An Inverse Betz MethodJournal of Aircraft, 1975
- Far-Field Wake-Vortex Characteristics of WingsJournal of Aircraft, 1975
- Rapid Scanning, Three-Dimensional Hot-Wire AnemometerSurveys of Wing-Tip VorticesJournal of Aircraft, 1973
- On the Inviscid Rolled-Up Structure of Lift-Generated VorticesJournal of Aircraft, 1973
- Remarks on vortex-lattice methods.Journal of Aircraft, 1973