Equivalence of the Spanwise Lift Distribution to the Spanwise Lift-Influence Function for Slender Wings and Wing Bodies
- 1 July 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (7), 503-504
- https://doi.org/10.2514/8.2016
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Remarks on Low-Aspect-Ratio Configurations in Supersonic FlowJournal of the Aeronautical Sciences, 1951
- The Minimum Drag of Thin Wings in Frictionless FlowJournal of the Aeronautical Sciences, 1951
- Some Recent Measurements in a Two-Dimensional Turbulent ChannelJournal of the Aeronautical Sciences, 1950
- The Reversal Theorem of Linearized Supersonic Airfoil TheoryJournal of Applied Physics, 1950
- Investigations of Velocity Fluctuations in a Turbulent FlowJournal of the Aeronautical Sciences, 1936