Wings with Minimum Drag Due to Lift in Supersonic Flow
- 1 January 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (1), 13-20
- https://doi.org/10.2514/8.8366
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Theoretical Investigation of the Flow Field About Blunt-Nosed Bodies in Supersonic FlightJournal of the Aerospace Sciences, 1958
- Turbulent Heat Transfer Through a Highly Cooled, Partially Dissociated Boundary LayerJournal of the Aerospace Sciences, 1958
- Transformation of the Compressible Turbulent Boundary LayerJournal of the Aerospace Sciences, 1958
- The Turbulent Boundary LayerPublished by Elsevier ,1956
- Experimental Investigation of Turbulent Boundary Layers in Hypersonic FlowJournal of the Aeronautical Sciences, 1955
- REDUCTION OF DRAG DUE TO LIFT AT SUPERSONIC SPEEDSPublished by Defense Technical Information Center (DTIC) ,1954
- Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of AttackJournal of the Aeronautical Sciences, 1952
- The Minimum Drag of Thin Wings in Frictionless FlowJournal of the Aeronautical Sciences, 1951