How the airplane wing cut through the exterior columns of the World Trade Center

Abstract The problem of the airplane wing cutting through the exterior columns of the World Trade Center is treated analytically. The exterior columns are thin-walled box beam made of high strength steel. The complex structure of the airplane is lumped into another box, but it has been found that the equivalent thickness of the box is an order of magnitude larger than the column thickness. The problem can be then modeled as an impact of a rigid mass traveling with the velocity of 240 m/s into a hollow box-like vertical member. The deformation and failure process is very local and is broken into three phases: shearing of the impacting flange; tearing of side webs; and tensile fracture of the rear flange. Using the exact dynamic solution in the membrane deformation mode, the critical impact velocity to fracture the impacted flange was calculated to be 155 m/s for both flat and round impacting mass. Therefore, the wing would easily cut through the outer column. It was also found that the energy absorbed by plastic deformation and fracture of the ill-fated column is only 6.7% of the initial kinetic energy of the wing.

[1]  Norman Jones,et al.  Dynamic response of a rigid plastic clamped beam struck by a mass at any point on the span , 1988 .

[2]  Werner Goldsmith,et al.  Non-ideal projectile impact on targets , 1999 .

[3]  Osamu Muragishi Premature cleavage of ship plating under reversed bending , 2000 .

[4]  Ew Parkes,et al.  THE PERMANENT DEFORMATION OF AN ENCASTRE BEAM STRUCK TRANSVERSELY AT ANY POINT IN ITS SPAN. , 1958 .

[5]  Tomasz Wierzbicki Concertina tearing of metal plates , 1995 .

[6]  Yu Jilin,et al.  Further experimental investigations on the failure of clamped beams under impact loads , 1991 .

[7]  C. R. Calladine,et al.  Inertia and strain-rate effects in a simple plate-structure under impact loading , 1991 .

[8]  N. Jones Plastic Failure of Ductile Beams Loaded Dynamically , 1976 .

[9]  Norman Jones,et al.  Response and Failure of Ductile Circular Plates Struck by a Mass , 1997 .

[10]  T. Wierzbicki,et al.  Impact response of a string-on-plastic foundation , 1992 .

[11]  A. Atkins,et al.  On Diverging Concertina Tearing , 1998 .

[12]  T. Wierzbicki,et al.  Multiple impact of beam-to-beam , 2005 .

[13]  G. G. Corbett,et al.  Impact loading of plates and shells by free-flying projectiles: A review , 1996 .

[14]  T. Wierzbicki,et al.  Transient response of an impulsively loaded plastic string on a plastic foundation , 1996 .

[15]  C. A. Calder,et al.  Plastic deformation and perforation of thin plates resulting from projectile impact , 1971 .

[16]  Tongxi Yu,et al.  A note on a ‘velocity sensitive’ energy-absorbing structure , 1989 .

[17]  N. Jones,et al.  Experimental investigation of clamped beams struck transversely by a mass , 1987 .