Determination of a Load Approaches for Aircraft Impacts - The Risks of Nuclear Energy Technology

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Fig. 14.24 Comparison of load functions according to RSK-LL, Boeing B747 and Airbus A320—

resulting total force

Fig. 14.25 Comparison of load functions according to RSK-LL, Boeing B747 and Airbus A320—

resulting total force divided by the particular impact area

Fig. 14.26 Comparison of load functions according to RSK-LL, Boeing B747 and Airbus A320 -

resulting total force divided by the particular perimeter

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