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I don't buy it, Wayne.  However, this input should give Ed an opportunity to 
regale us with yet another of his many conversations with Fred Weick on the 
subject. Don




________________________________
> From: [EMAIL PROTECTED]
> To: [EMAIL PROTECTED]; [EMAIL PROTECTED]; [email protected]
> Subject: Re: [COUPERS-FLYIN]
> Date: Mon, 16 Oct 2006 06:08:31 -0700
> 
> ----[Please read http://ercoupers.com/disclaimer.htm before following any 
> advice in this forum.]----
> Fellow Coupers::
> It has been a long time since I flew an Ercoupe without manual rudder control 
> input, but as I recomember it, the reason we want to let the nose strut to 
> fully extend upon touchdown is for the nosewheel to make terra-firma contact 
> at the same time as the main gear.  Done right in a crosswind, the nose wheel 
> will be aligned with the runway, and the aircrafts momentum, at the moment of 
> touchdown the strut begins to take the forward weight of the airplane and 
> compress, the robust main gear moves the aircraft line of thrust 
> configuration to the line of momentum, (The cross wind vector) the 
> controllable nose wheel slips gently though the fingers of the highly 
> experienced airframe controller, allowing the strut to fully compress, 
> causing a properly rigged Ercoupe tail to rise to 75 inches, and the negative 
> angle of incidence of the tail surface to effectively cause the aircraft to 
> quit flying, and pass on down the runway centerline bleeding off speed and 
> forward momentum in the process.
> Is that about right?
> Still doesn't answer the cable restraint question.  I never have figgured 
> that out, I think the nosewheel should be below the turbulent airstream 
> created by the propeller.  hence, no need for the cable at all, the 
> nutcracker does all the work of a restraint cable, that is if the bumper is 
> on correctly, and the nutcracker cannot go "over center."
> Wayne W.
> ----- Original Message -----
> From: Ed Burkhead<mailto:[EMAIL PROTECTED]>
> To: [EMAIL PROTECTED]<mailto:[EMAIL PROTECTED]> ; 
> Cflyin<mailto:[email protected]>
> Sent: Monday, October 16, 2006 5:17 AM
> Subject: RE: [COUPERS-FLYIN]
> ----[Please read http://ercoupers.com/disclaimer.htm before following any 
> advice in this forum.]----
> Dr. R. Beeman wrote:
> >>>>> If you land an Ercoupe on the mains in a crosswind and wait "...until 
> >>>>> the coupe itself swivels straight down the runway..." please tell me 
> >>>>> specifically what force will cause the aircraft to "swivel straight 
> >>>>> down the runway"?
> The answer is there is no magical force available to an Ercoupe or a spam can 
> for that matter. A spam can uses rudder to counteract the crab just before 
> touchdown, but a rudderless Ercoupe must use the runway itself to counteract 
> the crab, for if the Ercoupe pilot tries to take out the crab before touching 
> down, he'll simply fly away from the centerline.
> The only counterforce to a crosswind crab that a rudderless model of the 
> Ercoupe possesses is the force exerted through the nose wheel touching and 
> counteracting the cocked main gear. This is what the POH calls for and this 
> is all there is. There is no automatic swivel straight down the runway and if 
> you wait for it before planting your nose wheel you'll be cutting 
> daisies.<<<<<
> Doc,
> Please review Chapter 17 of Stick and Rudder, which in my copy starts on page 
> 312.
> Yes, there IS an automatic swivel, straight down the runway.
> The force that rotates the airplane to line up with the direction of travel 
> is exerted through friction with the ground.
> The friction vector comes at an angle along the direction of motion.  It can 
> be represented by two vectors at right angles, one along the longitudinal 
> axis of the aircraft and one directly sideways.
> |\
> | \
> |  \
> |   \
> |    \
> |     \
> |      \
> |       \
> -------à
> When touching down in the crab (whether the nose gear touches at the same 
> time or not), there is a side load on the tires – they are not lined up with 
> their motion.
> The tires do start to rotate and almost instantly stop providing resistance 
> along the vector of the aircraft’s longitudinal axis.  But, the frictional 
> push is at an angle and part of the force may be vector diagrammed as being 
> from the side of the aircraft.
> It is that side vector which pushes sideways on the main gear – and the main 
> gear is behind the aircraft’s center of gravity.  So, there’s a sideways push 
> on the rear of the aircraft.
> But, if the nose gear has already touched, any sideways vector on that is 
> almost instantly relieved because the nose gear will turn and align itself 
> with the direction of motion.  So, there’s no sideways push vector on the 
> front of the aircraft.  (This is why we must not hold the yoke firmly when 
> landing – a fingertips only grip will allow the nose gear to turn to line up 
> with its travel across the ground.)
> Summary:  There’s a sideways push to the rear of the aircraft but no sideways 
> push on the front of the aircraft.  So, the aircraft rotates.
> When the aircraft is in line with the direction of motion, all sideways 
> vectors disappear.
> Side notes:  the mass of the aircraft is concentrated near the center of 
> gravity.  The structures far from the center are light weight.  So, the 
> aircraft automatically rotates quickly.  The sideways force vector is 
> relieved quickly and is not very violent.  An egg in a saucer in your lap 
> will probably stay there. (Please use hard boiled eggs for your personal 
> testing.)  J
> If this isn’t adequate, I’ll try to hand draw, scan and send a proper vector 
> diagram of the forces involved later.  (I’ve got to get my daughter up and 
> get her to school.)
> Ed Burkhead
> http://edburkhead.com
> ed -at- edburkhead???.com          (change -at- to @ and remove "???")
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