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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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A Method For The Approximate Solution Of The Heat Equation
Author(s): Weiner, Jerome H.
Corporate Author(s): Institute Of Flight Structures,Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 54-427
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Thermal Stress Analysis For Aircraft Structures Part II. Bibliography
Author(s): Boley, Bruno A., Weiner, Jerome H.
Corporate Author(s): Institute Of Flight Structures, Department Of Civil Engineering and Engineering Mechanics, Columbia University.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-11
Report number: WADC TR 56-102 Part 2
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Thermal Stress Analysis For Aircraft Structures Theory And Methods Of Analysis
Author(s): Boley, Bruno A., Weiner, Jerome H., Tolins, Irwin S.
Corporate Author(s): Institute Of Flight Structures, Columbia University.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-08
Report number: WADC TR 56-102 Part 1
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Development of a One-Piece Plastic Windshield for High-Speed Aircraft
Author(s): Huff, Rolland D., Patrick, Stanley C., Frownfelter, Charles R.
Corporate Author(s): Goodyear Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-06
Report number: WADC TN 55-241 Part I
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Structural Design for Aerodynamic Heating Part III. Structural Design
Author(s): Dukes, W. H., Schintt, A.
Corporate Author(s): Bell Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-305 Part III
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Study Of Coiled Tubing For Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H., Stouffer, Ronald D.
Corporate Author(s): Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1955-02
Report number: WADC TR 55-121

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