The article describes the compliance evaluation of the glider cockpit crashworthiness numerical simulations with the static test. The design of the test and the numerical simulation model were prepared in accordance with JAR 22.561 (b)(2) requirements. The next part demonstrates suggestion of crashworthiness methodology evaluation of glider cockpit with help pilot injuries criteria. The whole simulation was developed using the nonlinear explicit transient dynamic computer code MSC. Dytran. The test and the simulations were carried out by the Institute of Aerospace Engineering, Brno University of Technology.
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