Influence of Hot-Wire Probe and Traverse on Low-Reynolds-Number Airfoil Experiments
Author:
Affiliation:
1. Mechanical and Mechatronics Engineering, University of Waterloo, Waterloo, Ontario N2L 3G1, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053311
Reference11 articles.
1. MuellerT. J. “Low Reynolds Number Vehicles,” AGARDograph 288, 1985.
2. CarmichaelB. H. “Low Reynolds Number Airfoil Survey,” NASA CR-165803, Vol. 1, 1981.
3. Effects of End Plates and Blockage on Low-Reynolds-Number Flows Over Airfoils
4. On the numerical near-wall corrections of single hot-wire measurements
5. The free shear layer tone phenomenon and probe interference
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