An experimental investigation of blade-vortex interaction at normal incidence
- 1 January 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (1) , 47-55
- https://doi.org/10.2514/3.45265
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Unsteady lifting-line theory as a singular perturbation problemJournal of Fluid Mechanics, 1985
- Aerodynamic theory for wing with side edge passing subsonically through a gustAIAA Journal, 1983
- The Rolling Up of the Trailing Vortex Sheet and Its Effect on the Downwash Behind WingsJournal of the Aeronautical Sciences, 1951