Calculation of profile drag of airfoils at low Mach numbers.
- 1 November 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 5 (6), 535-542
- https://doi.org/10.2514/3.43980
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Approximate Calculation of the Laminar Boundary LayerAeronautical Quarterly, 1949