The overturning response of an armored personnel carrier to air blast loads derived from a nuclear blast environment is presented. The orientation of the vehicle is side-on to the air blast shock front. It is assumed there is no translation at the downwind wheels, i.e., the roll over point. In addition, the vehicle is assumed to behave as a rigid body. That is, the suspension systems is taken as rigid, so that the wheels and axles rotate in unison with the body. It can be shown that this assumption slightly overestimates the overturning resistance of vehicles with suspension systems. For a stiff suspension system, such as that of the APC, the rigid body behavior assumption is justified. The only motion possible for this analysis is rotation about the rollover point. The effect of overturning restraint systems has been included in the analysis by incorporating a perfectly plastic vehicle to ground connection on the upwind side of the vehicle. The results give the threshold nuclear environment that just causes overturning. The threshold environment is given in terms of a peak overpressure corresponding to a weapon yield. Results are presented for a range of weapon yields from 1KT to 1MT.
Vehicle Overturning Vulnerability from Air Blast Loads
1984
10 pages
Report
No indication
English
Combat Vehicles , Nuclear Explosions & Devices , Armored personnel carriers , Rotation , Blast loads , Vulnerability , Roll , Shock resistance , Mathematical models , Yield(Nuclear explosions) , Nuclear explosion damage , Computerized simulation , Overturning resistance , OVRTRN computer program , Rollover , Component Reports