Vortex wakes of two transports measured in 80 by 120 foot wind tunnel
- 1 March 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 33 (2) , 399-406
- https://doi.org/10.2514/3.46951
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Validation of vortex-lattice method for loads on wings in lift-generated wakesJournal of Aircraft, 1995
- Wind-tunnel measurements of hazard posed by lift-generated wakesJournal of Aircraft, 1995
- The persistence of trailing vortices: A modeling studyPhysics of Fluids, 1995
- 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
- Rapid Scanning, Three-Dimensional Hot-Wire AnemometerSurveys of Wing-Tip VorticesJournal of Aircraft, 1973
- Aircraft Wake Turbulence and Its DetectionPublished by Springer Nature ,1971