Instantaneous flow field measurements of stalled regions on an oscillating airfoil
- 25 June 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- An improved experimental method to determine the complete Reynolds stress tensor with a single rotating slanting hot wireJournal of Physics E: Scientific Instruments, 1981
- Turbulence Structures in the Wake of an Oscillating AirfoilPublished by Springer Nature ,1981
- Unsteady Kutta Condition of a Plunging AirfoilPublished by Springer Nature ,1981
- Unsteady wake of a plunging airfoilPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Determination of the Reynolds-Stress Tensor With a Single Slanted Hot-Wire in Periodically Unsteady Turbomachinery FlowPublished by ASME International ,1979