Aerodynamics of Porpoising
Posted: 25 Mar 2022, 22:32
MOD EDIT: Split from this thread here - felt that it should kinda be split out into it's own thing
I wanted to bump this thread up and hear if Jin and Vyssion can comment on vortex shedding and aero elasticity and whether they can induce porpoising issues, especially in regards to the entire duct height being set by a sprung suspension with its own resonances.
Particular, honing in on this:
I wanted to bump this thread up and hear if Jin and Vyssion can comment on vortex shedding and aero elasticity and whether they can induce porpoising issues, especially in regards to the entire duct height being set by a sprung suspension with its own resonances.
Particular, honing in on this:
Especially in regards to how the underbody venturi represents a much larger share of the downforce, so the oscillations may have enough magnitude to induce the porpoising.I'm going to try... aerodynamics are not steady state, nice smooth contour plots in CFD and wind tunnel results are the result of long time averaging intervals. In reality the trailing edge flow will be as Vyssion showed 2 posts back - more akin to a Karman vortex street. Wing's are also not infinitely stiff so this may result in some oscillations which will affect pressure distribution - which will cause the wing to pitch and heave - but the oscillatory forces are rather small so it's unlikely to create very big deflections. However if you watched the Haas sharkfin and T-wing last year you'll see those unsteady effects can get quite big - even to the extent that parts fail because of it.