Calculation of Unsteady Transonic Aerodynamics for Oscillating Wings with Thickness
Open Access
- 1 October 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (10) , 601-608
- https://doi.org/10.2514/3.60396
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Interpolation using surface splines.Journal of Aircraft, 1972
- On the Calculation of Unsteady Nonlinear Three-Dimensional Supersonic Flow Past WingsJournal of Basic Engineering, 1968
- Solution of the transonic airfoil problem through parametric differentiation.AIAA Journal, 1967