A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Piloting
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

The Impossibility of Flying Heavy Aircraft Without Training



 
 
Thread Tools Display Modes
Prev Previous Post   Next Post Next
  #11  
Old March 3rd 06, 01:27 AM posted to rec.aviation.piloting,rec.aviation.homebuilt,rec.aviation.student
external usenet poster
 
Posts: n/a
Default lift, wings, and Bernuolli

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
 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) Rich Stowell Aerobatics 28 January 2nd 09 02:26 PM
UAV's and TFR's along the Mexico boarder John Doe Piloting 145 March 31st 06 06:58 PM
GAO: Electronic Warfa Comprehensive Strategy Needed for Suppressing Enemy Mike Naval Aviation 0 December 27th 05 06:23 PM
Washington DC airspace closing for good? tony roberts Piloting 153 August 11th 05 12:56 AM
USAF = US Amphetamine Fools RT Military Aviation 104 September 25th 03 03:17 PM


All times are GMT +1. The time now is 04:55 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.