[NSRCA-discussion] Aileron Differential

Bob Richards bob at toprudder.com
Sun Mar 9 07:09:04 AKDT 2008


When you are traveling at the speed of light, the headlights no longer function as headlights. They function as thrusters. :-)
   
  Bob R.
  

Matthew Frederick <mjfrederick at cox.net> wrote:
    .hmmessage P {   PADDING-RIGHT: 0px; PADDING-LEFT: 0px; PADDING-BOTTOM: 0px; MARGIN: 0px; PADDING-TOP: 0px  }  BODY.hmmessage {   FONT-SIZE: 10pt; FONT-FAMILY: Tahoma  }        OK... that made me laugh...
    ----- Original Message ----- 
  From: chris moon 
  To: nsrca-discussion at lists.nsrca.org 
  Sent: Saturday, March 08, 2008 6:10 PM
  Subject: Re: [NSRCA-discussion] Aileron Differential
  

Is this similar to traveling at the speed of light then turning on your headlights??


Ron Van Putte wrote:   
Nope.    Ron Van putte    On Mar 8, 2008, at 5:51 PM, Del Rykert wrote:      
  
Is there a Doppler effect if the ear listening is moving at the    same direction and speed as the source of the sound?  <g>        Del    ----- Original Message -----  From: "Ron Van Putte" <vanputte at cox.net>  To: "NSRCA Mailing List" <nsrca-discussion at lists.nsrca.org>  Sent: Saturday, March 08, 2008 6:37 PM  Subject: Re: [NSRCA-discussion] Aileron Differential        
  
Yeah, that and the Doppler Effect.    Ron Van Putte    On Mar 8, 2008, at 12:49 PM, Keith Hoard wrote:          
  
The Coriolis Effect . . . .    On Fri, Mar 7, 2008 at 5:53 PM, Nat Penton  <natpenton at centurytel.net> wrote:  Some of you guys covered the following in various ways.    There is drag due to lift because the lift vector ( force ) is not  perpendicular to the flight direction. Drag is a function of lift  and that component of the lift vector in the flight direction is  called induced drag.    Up, and down, both ailerons produce drag, but in unequal amounts if  the wing is in lift mode. The difference in drag for pattern  airplanes is small because of low wingloading ( low AOA ).    The symmetrical airfoil plays a role in keeping the drag  differential low because, to generate equal lift , upright to  inverted, requires a different AOA for the non-symmetrical section.    What did I forget?        Nat    _______________________________________________  NSRCA-discussion mailing list  NSRCA-discussion at lists.nsrca.org  http://lists.nsrca.org/mailman/listinfo/nsrca-discussion      
  --    Keith Hoard  Collierville, TN  khoard at gmail.com    _______________________________________________  NSRCA-discussion mailing list  NSRCA-discussion at lists.nsrca.org  http://lists.nsrca.org/mailman/listinfo/nsrca-discussion          

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