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Investigation of Certain Unsteady Aerodynamic Effects in Longitudinal Dynamic Stability
Author(s): Ashley, H., Zartarian, G., Neilson, D. O.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1951-12
Report number: AF TR 5986
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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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Destruction Tests Of Aircraft Structural Components; Part 2. Development Of A Single-Channel Bending Moment Measurement Method Applicable To A Complex Built-Up Structure For Both The Elastic And The Post-Buckling Regime Of Structural Response
Author(s): Criscione, Emanuel S., Ayvazian, Mi Hran, Wetmore, Kenneth R.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-09
Report number: WADC TR 54-385 Part 2
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Experimental Studies On The Postfailure Response Of A Simple Structural Model Subjected To Static And Dynamic Loading
Author(s): D'Amato, Richard
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-11-15
Report number: WADC TR 56-161
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Application Of The Variational Method, The Galerkin Technique, And Normal Coordinates In A Transient Temperature Distribution Problem
Author(s): Schmit, L. A.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-09
Report number: WADC TR 56-287
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Indicial Downwash And Its Structural Effect On The Horizontal Tail
Author(s): Hobbs, Norman P.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Report number: WADC TR 56-164

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