Abstract
Alternating pitch and heave of a foil can tap
Stability algebra of a foil free in pitch and elastic in heave is analytically solved for the first time to prove the stability contours of all Theodorsen frequencies radiate from the same super node of total imbalance and pitch inertia the same as for a virtual mass confined to the 3/4 chord point. The flutter frequency only involves these totals and the trail of the center of pressure behind the pitch axis. Oscillation is damped in the low ratios of total to virtual typical of hydrofoils in water but heavier- than-air wings can be unstable. High intrinsic pitch inertia ratio and trail decrease the tailheavy imbalance ratio needed to force pitch by heave. Perturbing the equations for heave varying as semi-rotary roll, an unswept wing of low enough dynamic imbalance ratio can start to flutter in light wind but stop and feather in storms. The dynamic imbalance can be reduced at large scale and low design windspeed where the gravity effect of static imbalance more safely forces pitch. Between starting and stopping, the amplitude ratio of pitch to roll drops, containing the rise with windspeed of the bending moment amplitude.
Get full access to this article
View all access options for this article.
