Skin Friction Measurements Using Oil Film Interferometry in the 11' Transonic Wind Tunnel at NASA Ames

Author:

Driver David1,Drake Aaron2

Affiliation:

1. NASA Ames Research Center

2. Northrop Grumman

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Measurement of skin friction distribution using oil film for industrial wind tunnels;Transactions of the Visualization Society of Japan;2021

2. Oil film interferometry technique for skin friction measurement in subsonic and supersonic flows;SPIE Proceedings;2015-06-22

3. Step Excrescence Effects for Manufacturing Tolerances on Laminar Flow Wings;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

4. Transition due to Surface Steps in the Presence of Favorable Pressure Gradients;26th AIAA Applied Aerodynamics Conference;2008-06-14

5. Oil-Film Interferometry Shear Stress Measurements in Large Wind Tunnels - Technique and Applications (Invited);24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2004-06-19

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