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 » Simulators
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

Lift and Angle of Attack



 
 
Thread Tools Display Modes
  #1  
Old August 6th 03, 07:22 PM
Peter Duniho
external usenet poster
 
Posts: n/a
Default

"Dave Daniels" wrote in message
...
[...] If the lift is constant, then
higher speeds require a smaller lift coefficient and therefore the
induced drag coefficient is smaller. Am I on the right track here?


Yes. It is, in fact, basically what all three respondents to your post
(myself included) said.


 




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
Tamed by the Tailwheel [email protected] Piloting 84 January 18th 05 04:08 PM
Newbie Qs on stalls and spins Ramapriya Piloting 72 November 23rd 04 04:05 AM
A very basic question Ramapriya Piloting 45 November 9th 04 01:57 PM
Rag and tube construction and computer models? BllFs6 Home Built 24 April 12th 04 12:20 PM
Angle of climb at Vx and glide angle when "overweight": five questions Koopas Ly Piloting 16 November 29th 03 10:01 PM


All times are GMT +1. The time now is 08:44 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2024, Jelsoft Enterprises Ltd.
Copyright ©2004-2024 AviationBanter.
The comments are property of their posters.