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Method For Predicting Dynamic Landing Loads
Author(s): Eisenman, Richard L., Kramer, Edward H.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-09
Report number: WADC TR 54-28
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Thermo-Elastic Stresses And Deflections In Beam-Columns
Author(s): Boley, Bruno A., Mechanic, Harold
Corporate Author(s): Institute Of Air Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-425
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Thermo-Elastic Stresses And Deflections In Thin-Walled Beams
Author(s): Boley, Bruno A., Tolins, Irwin S.
Corporate Author(s): Institute Of Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-12
Report number: WADC TR 54-426
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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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Flutter Characteristics of a T-Tail
Author(s): Pengelley, G. E., Wilson, L. E., Epperson, T. B., Ransleben, G. E.
Corporate Author(s): Southwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report number: WADC TR 52-162

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