On Wed 01 Sep, Frank & Lori Koegler wrote:
> What's "washout"?

  Ah, yes, should have explained that. A wing
  without washout is a wing where the reference
  line of the airfoil(s) used are perfectly
  aligned, no twist at all.
  
  As one wants to keep the wing tips maintaining
  lift as long as possible (as otherwise the flying
  becomes pretty much like balancing a ball on your head -
  pretty unstable and quite difficult). This affects the 
  placing of an aircraft's airbrakes, for instance, so they
  normally go inside the ailerons. In short, a good aircraft
  should have aileron control at all speeds - if possible. 
  If the aircraft is a polyhedral you should still aim for 
  that the tips stalls after the inner portion of the wing.
  
  So if the wing has some taper, or the profile towards the tip 
  stalls earlier (at a lower angle) than the root profile (this is
  often, but not always, the case), due to different thickness,
  or various other reasons, the normal solution is to twist the
  wing, so that the inner section has a greater angle than the tips.
  
  For instance, if you use Eppler profiles the twist should generally be 
  very little 0-2.5 degrees, depending on which taper and profiles you 
  use, while swept wings can have as much as 9-10 degrees (Miachev bombers)!
  
  The problem with washout is that while it can be used to tailor the lift
  distribution of a wing perfectly (an elliptical lift distribution
  is perfect on everything but flying wings), the washout will only 
  work perfectly for one speed!
  
  And aircraft with a lot of washout tend to have a very fixed maximum speed,
  as the wingtips on a very twisted wing will produce downforce at high speed,
  eventually breaking itself up if you pass maximum allowed speed. 
  So designers try to use as little as possible and instead play with 
  different airfoils, or making small changes to the basic airfoil towards 
  the wing tip (often added droop towards the tip - a classic addition to 
  later models of certain buizjets, as with such a relatively easy modification
  they can lower the minium speed on approach and take off, or increase
  gross weight, or both, with little cost.

  'Droop' in this context is a minute change to the nose of the airfoil, often
  by bonding a section to the basic wing. Even the mighty Avro Vulcan flew badly
  until quite a lot of droop was added on the outer wing panels!
  
  Hope this helped?

Tord,
Sweden

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Tord S. Eriksson, Ovralidsg.25:5, S-422 47 Hisings Backa, Sweden

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