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On Wed, 1 Mar 2006 at 22:43:58 in message
.com, " wrote: It discussed the Bernuolli theory of flight- and (if I recall) quite conclusively proved that one of the _fundamental_ assumptions of the Bernuolli theory- that air that travels path over the top of the wing is flowing appreciably faster than air that flows over the bottom- is simply incorrect in a compressible fluid.... There is not really a Bernoulli theory of lift. Bernoulli's theory shows the relationship between the velocity and pressure of fluid flow when energy is not added or removed and the flow is subsonic. It is a very simple theory which is correct for much of the time. It quite accurately, at lower speeds, represents the velocity and pressures between streamlines. The air does flow faster over the top than the bottom and for the lower subsonic region air behaves very closely to being incompressible. Generally pressure changes are transmitted at the velocity of sound. At high subsonic and of course at supersonic speed the effect of compressibility cannot be ignored. Shock waves form, first on places like the top surface of the wing where the air first reaches the velocity of sound. As the speed rises they become bigger and move towards the leading and trailing edges. Above Mach one the air does not detect the approaching aircraft! :-) I have just read a few more messages in this thread and discussing lift in this general way without maths and without using at least simple physics and slowly developing the methods is almost futile. What's it matter about lift as long as the aircraft fly? !!!!! -- David CL Francis |
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