On an Integral Equation in the Supersonic Oscillating Wing Theory
- 1 October 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (10), 724-726
- https://doi.org/10.2514/8.2811
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- A general solution for the rectangular airfoil in supersonic flowQuarterly of Applied Mathematics, 1953
- Purely Rolling Oscillations of a Rectangular Wing in Supersonic FlowJournal of the Aeronautical Sciences, 1951
- Source-superposition method of solution of a periodically oscillating wing at supersonic speedsQuarterly of Applied Mathematics, 1951
- Periodic Motions of a Rectangular Wing Moving at Supersonic SpeedJournal of the Aeronautical Sciences, 1950
- Time-dependent linearized supersonic flow past planar wingsCommunications on Pure and Applied Mathematics, 1950