Paper presents the numerical and the experimental results of an ongoing joint research program developed between academic partners and Piaggio Aero Industries to design a bird-impact resistant glass laminate structure used for typical aeronautical windshield. Detailed nonlinear transient finite element analysis was carried out using the explicit code MSC/DYTRAN.
FE study of windshield subjected to high speed bird impact / Guida, Michele; A., Grimaldi; Marulo, Francesco; A., Sollo. - ELETTRONICO. - ID ICAS 2008 9.4.3:(2008), pp. 1-8. (Intervento presentato al convegno 26th Congress Of The International Council Of The Aeronautical Sciences (26th ICAS) tenutosi a inglese nel September 13-19, 2008).
FE study of windshield subjected to high speed bird impact
GUIDA, MICHELE;MARULO, FRANCESCO;
2008
Abstract
Paper presents the numerical and the experimental results of an ongoing joint research program developed between academic partners and Piaggio Aero Industries to design a bird-impact resistant glass laminate structure used for typical aeronautical windshield. Detailed nonlinear transient finite element analysis was carried out using the explicit code MSC/DYTRAN.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
