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Muto, K.; Tachikawa, H.; Sugano, T.; Tsubota, H.; Kobayshi, H.; Kasai, Y.; Koshika, N.; Tsujimoto, T.
Transactions of the 10th international conference on structural mechanics in reactor technology1989
Transactions of the 10th international conference on structural mechanics in reactor technology1989
AbstractAbstract
[en] Structural damage induced by an accidental aircraft crash into a reinforced concrete structure includes local damage caused by the engine, the rigid portion of the aircraft, and the global elasto-plastic structural response caused by the entire aircraft. Local damage consists of spalling of concrete from the front face of the target together with missile penetration into the target, scabbing of concrete from the rear face of the target and perforation of the missile through the target. The engine is a soft missile that deforms during impact. An experimental research program has been planned and executed to establish a rational evaluation method of the local damage by the deformable engine missiles
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Source
Hadjian, A.H. (Bechtel Power Corp., Los Angeles, CA (USA)); Extreme loads analysis; 337 p; ISBN 0-9623306-0-4; ; 1989; p. 257-264; American Association for Structural Mechanics in Reactor Technology; Los Angeles, CA (USA); 10. international conference on Structural Mechanics in Reactor Technology (SMIRT); Anaheim, CA (USA); 14-18 Aug 1989; CONF-890855--; American Association for Structural Mechanics in Reactor Technology, P.O. Box 60860, Los Angeles, CA 90060 (USA)
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Book
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Conference
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