Experiments on a Laminar Suction Airfoil of 17 Per Cent Thickness
- 1 April 1949
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 16 (4) , 227-236
- https://doi.org/10.2514/8.11771
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- The Use of Damping Screens for the Reduction of Wind-Tunnel TurbulenceJournal of the Aeronautical Sciences, 1947
- Laminar Boundary-Layer Oscillations and Stability of Laminar FlowJournal of the Aeronautical Sciences, 1947
- Verhinderung des Turbulentwerdens einer Grenzschicht durch AbsaugungThe Science of Nature, 1941
- Some Modern Methods of Research in the Problems of FlightJournal of the Royal Aeronautical Society, 1939
- Flight Experiments on the Boundary LayerJournal of the Aeronautical Sciences, 1938