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- W2321820184 abstract "An analytical method has been developed for assessing crash dynamics of large transport aircraft, such as in the NASA Controlled Impact Demonstration (CID) jet crash test on December 1, 1984. The DYCAST nonlinear finite-element computer code was used in a series of progressively more difficult tasks to model complete transport aircraft crashes. Single aircraft frames and fuselage section vertical drop tests were modeled and analyzed to obtain comparisons with experimental data and to develop hybrid element crash springs for use in the large CID model. Predictions of crash and acceleration levels from a symmetric CID model agreed well with data from the CID experiment." @default.
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- W2321820184 date "1986-05-19" @default.
- W2321820184 modified "2023-09-27" @default.
- W2321820184 title "Structural analysis of the controlled impact demonstration of a jet transport airplane" @default.
- W2321820184 cites W1569938303 @default.
- W2321820184 doi "https://doi.org/10.2514/6.1986-939" @default.
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