Well, since that thread I've discovered the Drag Equation and am now able to make some rough calcs.
I'm answering whether or not a nuclear blast could tip an AT-AT.
I can plug these into the drag equation and then divide the tipping impulse by the result, to see how long an AT-AT could last in supersonic wind. Keep in mind, that I'm not factoring in increased air tempurature and pressure caused by a nuclear blast. The figures may be inaccurate, so I'm open to correctionOn Wed Dec 22, 2004 4:18 pm, I wrote: AT-AT overbalancing torque:
2.45E7Nm
AT-AT overblancing impulse/momentum:
1.1E7Ns
Density of air:
1.225kg/m^3
Speed of sound in air:
320m/s IIRC
Approximate surface area of AT-AT's side:
100m²
I assume that the side of the AT-AT has a drag coefficient of 2 as most rectangles with these dimensions are close to this. The Cd may be higher, since the head is rather oddly shaped. But, having a Cd of two cancels out the 1/2 part of the equation.
So, we have 1.225*320²*100=12 544 000 N lower limit, since I'm assuming that airspeed is limited to the speed of sound.
Then I divide the tipping impulse by that and according to their quotient, the AT-AT, would only last 0.87 seconds in supersonic wind. If it had advance warning and was able to kneel to three metres above the ground, it would only last 1.56 seconds.
So, if winds were to sustain for at least one second, an AT-AT could be knocked over, as Walper suggested. That is, if I'm not mistaken, since my figures are a bit questionable.