Global/local analysis of composite light aircraft crash landing
2003; Elsevier BV; Volume: 81; Issue: 8-11 Linguagem: Inglês
10.1016/s0045-7949(02)00401-7
ISSN1879-2243
Autores Tópico(s)Dynamics and Control of Mechanical Systems
ResumoThe objective of this paper is to present the implementation of so-called global/local approach to crash landing analysis of the light composite aircraft. The analyses and experimental verifications have been performed for PZL I-23 aircraft, designed jointly by Institute of Aviation and PZL Swidnik aircraft factory. Some criteria for designing the light composite aircraft, according to the “safe-crash” rule have been formulated.
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