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Effects of Airplane Elasticity and Unsteady Flow on Longitudinal Stability
Author(s): Goland, Martin, Luke, Tudell L., Sacks, Irving
Corporate Author(s): Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1953-11
Report number: WADC TR 53-425
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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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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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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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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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Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail
Author(s): Hoffman, Niles R., Spielberg, Irvin N.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-53
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Theoretical Studies of the Effects of Aspect Ratio on Flutter
Author(s): Goland, Martin, Luke, Y. L., Dengler, M. A.
Corporate Author(s): Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report number: WADC TR 54-29
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Subsonic Flutter Model Tests of Wings Carrying Heavy Tip Pods. Part 2. Swept Wings
Author(s): Brady, W. G., Maier, H. G., Pargoff, Walter T.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report number: WADC TR 53-161 Part 2
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Coiled Stainless Steel Tubing: Part I. Test Results
Author(s): Chmura, Joseph J., Jr., Stouffer, Ronald D., Winter, Albert N.
Corporate Author(s): Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1957-07
Report number: WADC TR 57-507 Part I

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