Wouldn't the high velocity of the exhaust be resistant, for a small distance after leaving the tip, to forming a vortex?
Brian
I'm inclined to agree. The trailing vortices behind a 747 (for example) form fully some way aft of its tailplane. The delay is often observable from the ground when an aircraft is "contrailing" at high altitudes. Aircraft that operate at high incidences, such as the F16 look-alike posted by n smikle, are different. Here the principal vortex forms as shown in his diagram. However, in that case the vortex travels over the wing some distance above it (which it must do to maintain the circulation). I happen to know that because I once spent some interesting times chasing an HP 115 trying to fly through its trailing vortices in order to measure their velocity profile. "Vortex" lift generation trades efficiency (lower L/D) for robustness (the wing won't stall).hardingfv32 wrote:Wouldn't the high velocity of the exhaust be resistant, for a small distance after leaving the tip, to forming a vortex?
Hmm interesting that you mention that. It could be the reason why the RedBull ride height in the rear is much higher than the others.However, in that case the vortex travels over the wing some distance above it (which it must do to maintain the circulation). I happen to know that because I once spent some interesting times chasing an HP 115 trying to fly through its trailing vortices in order to measure their velocity profile. "Vortex" lift generation trades efficiency (lower L/D) for robustness (the wing won't stall).