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"B Lacovara" wrote in message
... I've been under the impression that the biggest gain in ground effect is cutting off the tip vortices thus significantly reducing drag. Could be dangerous for me to try to interpret Hoerner (in "Fluid Dynamic Lift"), but the effect on the vortices is indirect, as it's more relevantly the downwash behind the wing which is being altered and therefore induced angle of attack, and hence drag. He thus measures and graphs the height above the ground as the height from the trailing edge. There's really no "cushion" of air involved, as the pressure of the air under the wing can be zero or negative with respect to free-stream air, per normal except at high lift coefficients, and wing can still exhibit ground effect. Fred F. |
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