Thick supercritical airfoils with low drag and natural laminar flow
- 1 June 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 24 (6), 405-411
- https://doi.org/10.2514/3.45460
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Development of modern airfoil sections for high subsonic cruise speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Supercritical Wing Sections IIIPublished by Springer Science and Business Media LLC ,1977
- BOUNDARY LAYER TRANSITION- FREESTREAM TURBULENCE AND PRESSURE GRADIENT EFFECTSAIAA Journal, 1963