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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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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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5 items

Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast-Type Profiles In The Shock Tube By The Reflection Method

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

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

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

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

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