Transient Aerodynamics Of Two-Dimensional Airfoils, Part 2. Interferometric Measurements Airflow Development About An Naca 65-101 Airfoil In Shock-Initiated Subsonic Flow, Including Transient Stalling Effects

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Report Number: WADC TR 54-368 Part 2
Author(s): Ruetenik, J. Ray, Witmer, Emmett A.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory and Aero Medical Laboratory
Date of Publication: 1956-03
Pages: 102
Contract: AF 33(616)-2359
DoD Project: 1350
DoD Task: 13605
Identifier: AD0151018

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Provenance: IIT

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