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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
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
Report number: WADC TR 54-368 Part 2
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Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast-Type Profiles In The Shock Tube By The Reflection Method
Author(s): Lee, Robert C. K., Witmer, Emmett A., Ruetenik, J . RayCorporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Report number: WADC TR 54-383 Part 1
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Transient Aerodynamics Of Two-Dimensional Airfoils, Part 1 - Interferometric Measurements Of Two-Dimensional Airflow Development About A Symmetrical Double-Wedge Airfoil In Shock-Initiated Subsonic Flow
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: 1956-08
Report number: WADC TR 54-368 Part 1
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Dynamic Response of Shells to Externally-Applied Dynamic Loads
Author(s): Leech, John W., Pian, T. H. H., Witmer, Emmett A., Herrmann, WalterCorporate Author(s): Massachusetts Institute of Technology
Date of Publication: 1962-11
Report number: ASD TDR 62-610
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