Go Back  PPRuNe Forums > Flight Deck Forums > Tech Log
Reload this Page >

reversers and a/c speed

Tech Log The very best in practical technical discussion on the web

reversers and a/c speed

Old 6th Jan 2011, 21:21
  #121 (permalink)  
Join Date: Dec 2006
Location: The No Trangression Zone
Posts: 2,049
Pugilistic Animus

Seeing is believing....

YouTube - F-35 Take Off & Landing

Turbine D
then how do you resolve this conundrum?:

Alphai =180/pi (b/2pi)d/dy(cl*c/4b)dy/(yi-y) integrated between the semi-span bounds b/2 and -b/2....

oh for the F-35?

I'll take a chance and use Guppy's answer..as it is always correct

No change. Again, raw thrust for vertical flight; the aircraft does not rise by producing airflow and blowing it over it's own wings to produce lift.

Still does nothing to illustrate PBL's argument.
We need a break

Last edited by Pugilistic Animus; 9th Jan 2011 at 20:29. Reason: lowercase 'cl and c'...ay ay ay
Pugilistic Animus is offline  

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

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are Off
Refbacks are Off

Thread Tools
Search this Thread

Contact Us Archive Advertising Cookie Policy Privacy Statement Terms of Service

Copyright 2018 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.