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Showing 1 to 1 of 1 for “"slam, drop test"”.
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Validation of Seaplane Impact Load Theory and Structural Analysis of the Martin 270
<p>Flight and drop tests of the Martin 270 (M270) seaplane were conducted in 1955. Theoretical and empirical pressures were determined by use of Wagner’s theory and also by the Code of Federal Regulations (CFR). The pressure results from the experimental tests on the hull were compared with …