An analysis of the fatigue life of an airplane wing structure under overload conditions / by Abbott A. Putnam and Thomas D. Reisert.
Results of an analysis to determine the effect of overload operation on wing fatigue life are presented. The investigation was confined to one transport-type airplane, which was assumed to operate at cruising power and with overload up to 50 percent of design gross weight.
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Other title: | NACA Wartime Reports. Series L. |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1946]
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Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L10. |
Subjects: |
Norlin Library - Basement - Government Information - US
Call Number: |
Y 3.N 21/5:11/L10
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Y 3.N 21/5:11/L10 | Available Place a Hold |