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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 . Ray
Corporate 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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The Effects Of Thermal Radiation On Aircraft Structures, Part 3. Structural Behavior Of Box-Beams Under Combined Static And Thermal Loads

Author(s): Loria, John C., Mar, James W., Engel, Seymour J.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1957-06

Report number: WADC TR 54-384 Part 3

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The Effects Of Thermal Radiation On Aircraft Structures, Part I. The M.I.T. Mark I Radiant Heating Structural Test Facility

Author(s): Loria, John C., Mar, James W., Blackstock, William J.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1954-10

Report number: WADC TR 54-384 Part 1

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Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks

Author(s): McCarthy, John F., Jr., Martuccelli, John R., Asher, Gifford W., Zartarian, Garabed
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12

Report number: WADC TR 54-113 Part 2

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Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces

Author(s): Asher, Gifford W., Weatherhill, Warren H.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01

Report number: WADC TR 54-113 Part 3

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Optical Methods Of Measuring Plasma Jet Temperatures

Author(s): Hottel, H. C., Jensen, W. P., Williams, G. C.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Materials Laboratory
Date of Publication: 1961-06

Report number: WADD TR 60-676

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Remarks

Author(s): Draper, C. S.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Flight Control Laboratory
Date of Publication: 1961-03

Report number: WADC TR 59-49 p. 55-57

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Massachusetts Institute of Technology Presentation

Author(s): Whitaker, H. Philip
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Flight Control Laboratory
Date of Publication: 1961-03

Report number: WADC TR 59-49 p. 58-78

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