Effects of Leading-Edge Separation on Thin Wings in Two-Dimensional Incompressible Flow
- 1 August 1957
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (8) , 597-604
- https://doi.org/10.2514/8.3915
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The slender elliptic cone as a model for non-linear supersonic flow theoryJournal of Fluid Mechanics, 1956
- Note on the Motion Inside a Region of Recirculation (Cavity Flow)Journal of the Royal Aeronautical Society, 1956
- Types of Flow on Swept Wings With Special Reference to Free Boundaries and Vortex SheetsJournal of the Royal Aeronautical Society, 1953
- Investigations of the Turbulent Mixing Regions Formed by JetsJournal of Applied Mechanics, 1935