Flying-Hot-wire Study of Flow Past an NACA 4412 Airfoil at Maximum Lift
- 1 April 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (4), 321-329
- https://doi.org/10.2514/3.61127
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Features of a separating turbulent boundary layer in the vicinity of separationJournal of Fluid Mechanics, 1977
- Experimental investigation of subsonic turbulent separated boundary layers on an airfoilJournal of Aircraft, 1977
- A study of the constant-temperature hot-wire anemometerJournal of Fluid Mechanics, 1971