Numerical Analyses of a Shield Building Subjected to a Large Commercial Aircraft Impact

Table 1

Mass distribution of a Boeing 767-200ER.

Type	Part	Fuselage	Wing	Engine	Empennage	Fuel	Cargo	Total
Aircraft A	Mass (ton)	53.97	16.78	8.75	2.7	31.3	—	113.5
Aircraft B	Mass (ton)	53.97	16.78	8.75	2.7	73.36	23.63	179.19