Rapid Scanning, Three-Dimensional Hot-Wire AnemometerSurveys of Wing-Tip Vortices
- 1 December 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (12) , 752-757
- https://doi.org/10.2514/3.60301
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Study of the far wake vortex field generated by a rectangular airfoil in a water tankPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Wind-Tunnel Studies of Wing Wake TurbulenceJournal of Aircraft, 1972
- The farfield structure of aircraft wake turbulencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Analytical studies of aircraft trailing vorticesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- An Analysis of Flight Measurements in the Wake of a Jet Transport AircraftPublished by Springer Nature ,1971
- Decay of a Vortex Pair behind an AircraftPublished by Springer Nature ,1971
- An Experimental Investigation of Trailing Vortices Behind a Wing with a Vortex DissipatorPublished by Springer Nature ,1971
- Structure of trailing vortices.Journal of Aircraft, 1968
- Turbulent line vorticesJournal of Fluid Mechanics, 1963