- #1
ThePeculiarEngineer
Homework Statement
The single wheel of an aircraft can undergo a max of 7500N at a vertical velocity of 8 m/s on landing. The vertical spring moves in SHM and has a stiffness of 600N/mm. The systems vertical damper has a damping coefficient of 38 x 10^3 Ns.m-1
Homework Equations
F=Kx
F=Kx+cv=ma
ω = √ k/m
The Attempt at a Solution
I've tried "F=Kx+cv=ma" but when i solve for "Kx+cv" I am not quite sure how to then solve for the mass. the question doesn't even give the mass