Afternoon STW,
I’m undertaking a project as part of a group and have elected to cover the suspension analysis of a monarch RT3 debonair.
I’m trying to generate a Force/Displacement diagram for the shock, but I’m struggling to work out the most accurate way to model it, so any help would be greatly appreciated.
From the ideal gas law, PV=nRT so to model the shock with adiabatic, isothermal compression it is possible to use Boyle’s Law:
P1V1=P2V2
i.e. volume is inversely proportional to pressure.
Obviously the air spring does not compress at constant temperature, so I’ve added the adiabatic gas constant to the equation which as far as I can tell, accounts for the temperature changes.
This leaves me with:
P1V1^1.4=P1V2^1.4
Which I then combined with F=P*A and did some rearranging of sorts, so to work out the force of the air on the piston for any given position in the stroke:
F=(Area of piston head)x(initial pressure)x(Initial Volume/(Initial Volume-Change in Volume)^1.4)
Is this a reasonable way to model the air spring or is there a better formula someone can direct me towards?
I plan to use this method to model the force of the positive spring and negative spring independently and subtract the negative from the positive.
I’m likely to have to estimate the actual dimensions of the shock too so if anyone had any technical data for a monarch shock it would be very handy!
I’ll also probably have a go at trying to model the dampers and including the static friction for the final graph but I haven’t got that far yet.
Thanks in advance for any info!