I'm not desperately doing anything, I did not mis-speak, and you should quit while you are behind.kilcoo316 wrote:Adrian Newby wrote:You do that. And they will laugh at you.I'll have to remember to tell the stressers that next time they go to calculate the loads on wing spars.
Wing spars do not have a support at each end.
Go draw yourself out a little shear force diagram of the estimated load across the wishbone.
Then draw out a bending moment diagram.
Then, draw out a point load on the wishbone which represents all the aerodynamic loading through a single point - the centre of pressure.
See the distance from the centre of pressure to either end - those are the effective lever arms that will tell you what proportion of load will be sent to the car's springs and what proportion will go directly to the upright.
Your desperately trying to trip me up to hit back for your mis-speak earlier (I don't really know why, is your ego that delicate?). But to be honest your failing miserably.
Put a board across two saw horses. Pull down on the board anywhere between the two saw horses. There is no lever.