Aerodynamic characteristics of slender wings with sharp leading edges - A review
- 1 March 1976
- journal article
- review article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (3) , 161-168
- https://doi.org/10.2514/3.44517
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Extension of a Vortex-Lattice Method to Include the Effects ofLeading-Edge SeparationJournal of Aircraft, 1974
- A Conceptual Study of Leading-Edge-Vortex Enhancement by BlowingJournal of Aircraft, 1974
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Numerical lifting-surface theory - Problems and progressPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- A THEORY FOR THE LOW-SPEED AERODYNAMICS OF STRAIGHT AND SWEPT WINGS WITH FLOW SEPARATIONPublished by Defense Technical Information Center (DTIC) ,1963
- Experimental Pressure Distributions on Oscillating Low Aspect Ratio WingsJournal of the Aeronautical Sciences, 1956
- Leading-Edge Separation from Delta Wings at Supersonic SpeedsJournal of the Aeronautical Sciences, 1953
- A Theory for Rectangular Wings of Small Aspect RatioJournal of the Aeronautical Sciences, 1937