Unseeded Velocity Measurements Around a Transonic Airfoil Using Femtosecond Laser Tagging

Author:

Burns Ross A.1,Danehy Paul M.1

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference30 articles.

1. LadsonC. L.RayE. J. “Evolution, Calibration, and Operational Characteristics of the Two-Dimensional Test Section of the Langley 0.3-Meter Transonic Cryogenic Tunnel,” NASA TP-2749, 1987.

2. SnowW. L.BurnerA. W.GoadW. K. “Image Degradation in Langley 0.3-Meter Transonic Cryogenic Tunnel,” NASA TM 84550, 1982.

3. SnowW. L.BurnerA. W.GoadW. K. “Improvement in the Quality of Flow Visualization in the Langley 0.3-Meter Transonic Cryogenic Tunnel,” NASA TM-87730, 1987.

4. BatillS. M. “Experimental Uncertainty and Drag Measurements in the National Transonic Facility,” NASA CR 4600, 1994.

5. Advanced Measurement Techniques for High Reynolds Number Testing in Cryogenic Wind Tunnels

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