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reversers and a/c speed

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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
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