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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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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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The Temperature Response Of Thick Plates Exposed To Radiant Heat Pulses
Author(s): Loria, John C., Schmit, Lucien A.
Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-07-25
Report number: WADC TR 56-149

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