[sci.military] Soviet Wing in Ground-effect Machine?

raymond%europa@uunet.UU.NET (Raymond Man) (07/28/90)

From: raymond%europa@uunet.UU.NET (Raymond Man)

In <1990Jul25.004935.7662@cbnews.att.com>William Carroll discussed
areodynamics of WIG vehicle. The effect ot a jet tending to attach
to a surface is called the coanda effect, after the Italian Henri
Coanda, who BTW was the designer of the first vector thrust 
aeroplane, which has the engine (and prop) tilted to change the thrust line
and was burnt down because the hot exhaust lit up the fabric
of the fuselage when the hot jet stayed on the surface due to, of course,
the coanda effect.

The WIG mainly reduces the induce drag on the wing, which sees a mirror
image of itself giving out tip vortices or the opposite sense. In simpler
terms, since the lower surface pressure is higher than the upper, leakage
to the top occurs aroung the wing tip generating a tip vortex which 
accounts for the lost of energy due to lift induced drag. The closer is the
wing  to the ground, the smaller the area for such leakage flow and the
weaker is the vortex. So a WIG vehicle can use a structurally efficient
stubby wing without the penalty of large induced drag due to a low
effective aspect ratio.
Just call me `Man'. 
"And why take ye thought for "    --   Matt. 6:28
raymond@jupiter.ame.arizona.edu