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- W600895093 abstract "Two assumptions are made in the analytical method for determining the transient stresses in airplane structures during landing. The first assumption, that the landing impact forces are independent of the response of the structure, is justified by a simple analytical study. The second assumption, that the damping and aerodynamic forces can be neglected, is verified by comparing the results of wind-on and wind-off drop tests of a model wing in a wind tunnel. The total transient stress is considered to be the sum of the stresses that would result if the system were restrained against vibrating and the additional stresses that result from the vibratory motion. This method has been made more suitable for practical application by the use of a transient analyzer. The drop tests also provide an experimental check on the analytical method." @default.
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- W600895093 date "1950-12-01" @default.
- W600895093 modified "2023-09-26" @default.
- W600895093 title "Analytical and Experimental Studies on Dynamic Loads in Airplane Structures During Landing" @default.
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- W600895093 doi "https://doi.org/10.2514/8.1804" @default.
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