The Two-Dimensional Incompressible Aerodynamic Coefficients for Oscillatory Changes in Airfoil Camber
- 1 June 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (6) , 432-434
- https://doi.org/10.2514/8.2665
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Stabilization of Shock Waves in Channel FlowJournal of the Aeronautical Sciences, 1950