Femtosecond Laser Electronic Excitation Tagging Velocimetry in a Transonic, Cryogenic Wind Tunnel

Author:

Burns Ross A.,Danehy Paul M.,Halls Benjamin R.,Jiang Naibo

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference15 articles.

1. The National Transonic Facility - A research retrospective

2. 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.

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

4. 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.

5. GartrellL. R.GooderumP. B.HunterW. W.MeyersJ. F. “Laser Velocimetry Technique Applied to the Langley 0.3-Meter Transonic Cryogenic Tunnel,” NASA TM-81913, 1981.

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