Maximum lift-to-drag ratio airfoils at moderate supersonic speeds.
- 1 March 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (3), 471-477
- https://doi.org/10.2514/3.5131
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Maximum lift-to-drag ratio airfoils at moderate supersonic speeds.AIAA Journal, 1969
- Base drag effects on maximum lift-to-drag ratio airfoils at moderate supersonic speedsJournal of Optimization Theory and Applications, 1969
- On the minimization of the product of the powers of several integralsJournal of Optimization Theory and Applications, 1967