Rotating cylinder for circulation control on an airfoil
- 1 July 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Hydronautics
- Vol. 10 (3), 102-105
- https://doi.org/10.2514/3.48147
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Leading-edge rotating cylinder for boundary-layer control on lifting surfacesJournal of Hydronautics, 1975
- Flight performance of a circulation controlled STOLPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A subsonic diffuser with moving walls for boundary-layer control.AIAA Journal, 1973
- A Calculation Method for Circulation Control by Tangential Blowing Around a Bluff Trailing EdgeAeronautical Quarterly, 1968
- THE EFFECT OF A ROTATING CYLINDER AT THE LEADING AND TRAILING EDGES OF A HYDROFOILPublished by Defense Technical Information Center (DTIC) ,1963
- The Magnus Effect: A Summary of Investigations to DateJournal of Basic Engineering, 1961
- Low-Drag and Suction AirfoilsJournal of the Aeronautical Sciences, 1948