Europa-List Digest Archive

Fri 09/09/16


Total Messages Posted: 3



Today's Message Index:
----------------------
 
     1. 05:11 AM - Adjusting Angle of Incidence (tonyvaccarella)
     2. 06:17 AM - Re: Adjusting Angle of Incidence (William Daniell)
     3. 02:02 PM - Re: Adjusting Angle of Incidence (Tim Ward)
 
 
 


Message 1


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    Time: 05:11:15 AM PST US
    Subject: Adjusting Angle of Incidence
    From: "tonyvaccarella" <tony@weimagine.com.au>
    Hi All, After finally getting my wings on again, I checked the Angle of Incidence to find that the port wing measures 2.5 degrees - as expected but the starboard wing measures 2.4 degrees. What I would like to know is how do you adjust the angle when the forward (W27) and aft sockets (W26) have already been bonded in place. From my investigations today, I believe that the leading edge pin and socket on the starboard wing needs to come up a fraction. I expect this is not the first time someone has had to make this adjustment and Im interested what solutions have been used by members of this forum. Many thanks Tony Sydney Australia S/N A011 -------- Tony Vaccarella Mascot NSW 2020 Sydney Australia Read this topic online here: http://forums.matronics.com/viewtopic.php?p=460370#460370


    Message 2


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    Time: 06:17:30 AM PST US
    From: William Daniell <wdaniell.longport@gmail.com>
    Subject: Re: Adjusting Angle of Incidence
    Tony I spoke to bud about this on my visit to his facility. It might be worth calling him. But basically he said that even if you build perfectly the incidence may change with finishing. Also that composite shifts over time. My build is like yours .1 off. I plan to add vg to soften the stall. Will On Sep 9, 2016 07:14, "tonyvaccarella" <tony@weimagine.com.au> wrote: > > > > Hi All, > > After finally getting my wings on again, I checked the Angle of Incidence > to find that the port wing measures 2.5 degrees - as expected but the > starboard wing measures 2.4 degrees. > > What I would like to know is how do you adjust the angle when the forward > (W27) and aft sockets (W26) have already been bonded in place. From my > investigations today, I believe that the leading edge pin and socket on the > starboard wing needs to come up a fraction. > > I expect this is not the first time someone has had to make this > adjustment and Im interested what solutions have been used by members of > this forum. > > Many thanks > Tony > Sydney Australia > S/N A011 > > -------- > Tony Vaccarella > Mascot NSW 2020 > Sydney Australia > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=460370#460370 > >


    Message 3


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    Time: 02:02:38 PM PST US
    Subject: Re: Adjusting Angle of Incidence
    From: Tim Ward <ward.t@xtra.co.nz>
    Tony, That may even be ideal as the aircraft tends to bank slightly left more so when you are the only one on board left seat due to slipstream effect and weight. I have a port aileron tab to keep wing level. Big vertical stabiliser and rudder gives the slipstream from prop rotating clockwise a left yaw increasing lift on right wing roll port. That's a theory. TIM Sent from my iPhone > On 10/09/2016, at 12:02 AM, tonyvaccarella <tony@weimagine.com.au> wrote: > > > Hi All, > > After finally getting my wings on again, I checked the Angle of Incidence to find that the port wing measures 2.5 degrees - as expected but the starboard wing measures 2.4 degrees. > > What I would like to know is how do you adjust the angle when the forward (W27) and aft sockets (W26) have already been bonded in place. From my investigations today, I believe that the leading edge pin and socket on the starboard wing needs to come up a fraction. > > I expect this is not the first time someone has had to make this adjustment and Im interested what solutions have been used by members of this forum. > > Many thanks > Tony > Sydney Australia > S/N A011 > > -------- > Tony Vaccarella > Mascot NSW 2020 > Sydney Australia > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=460370#460370 > > > > > > > > > >




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