X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from nschwmtas04p.mx.bigpond.com ([61.9.189.146] verified) by logan.com (CommuniGate Pro SMTP 6.0.5) with ESMTP id 6316116 for lml@lancaironline.net; Sun, 09 Jun 2013 21:01:30 -0400 Received-SPF: pass receiver=logan.com; client-ip=61.9.189.146; envelope-from=frederickmoreno@bigpond.com Received: from nschwcmgw08p ([61.9.190.168]) by nschwmtas04p.mx.bigpond.com with ESMTP id <20130610010053.DACW2030.nschwmtas04p.mx.bigpond.com@nschwcmgw08p> for ; Mon, 10 Jun 2013 01:00:53 +0000 Received: from Razzle ([58.170.118.157]) by nschwcmgw08p with BigPond Outbound id mR0o1l00P3PqZFe01R0qCi; Mon, 10 Jun 2013 01:00:53 +0000 X-Authentication-Info: Submitted using ID frederick.moreno@bigpond.com X-Authority-Analysis: v=2.0 cv=LvIQOwhc c=1 sm=1 a=JAITpso0j1fe2s0LYxaGaQ==:17 a=v1ivN9LTxp0A:10 a=JDadKst33uMA:10 a=8nJEP1OIZ-IA:10 a=1IlZJK9HAAAA:8 a=jZSARp0TQh0A:10 a=hslOrHpUAAAA:8 a=Ia-xEzejAAAA:8 a=3oc9M9_CAAAA:8 a=CjxXgO3LAAAA:8 a=XAPGKDdCAAAA:8 a=5FIZSGrRAAAA:8 a=zrDG9CcMAAAA:8 a=69EAbJreAAAA:8 a=1JXNnX0CAAAA:8 a=Nkm2IvvshJqAl0EE6voA:9 a=wPNLvfGTeEIA:10 a=-ZBvsNeBbbMA:10 a=ItdIRbnKRL4A:10 a=wR8WdYEwGqoA:10 a=zc6lhsSWC8gA:10 a=EzXvWhQp4_cA:10 a=U8Ie8EnqySEA:10 a=rC2wZJ5BpNYA:10 a=SvQ52vU_ylgA:10 a=EfJqPEOeqlMA:10 a=KNfte85PAAAA:8 a=7O5q-qACfdEF-NZ1iQEA:9 a=_W_S_7VecoQA:10 a=tXsnliwV7b4A:10 a=8m6LRutVOowA:10 a=b2fj0k-BPVZgzO83:21 a=x0mLEhdcI6ghJkqIEpcA:9 a=HXjIzolwW10A:10 a=dvIeMUh3dxkolpdY:18 a=JAITpso0j1fe2s0LYxaGaQ==:117 MIME-Version: 1.0 Message-Id: <51B52588.000033.04236@RAZZLE> Date: Mon, 10 Jun 2013 09:02:00 +0800 Content-Type: Multipart/related; charset="iso-8859-1"; type="multipart/alternative"; boundary="------------Boundary-00=_C7K5SBX3LVC000000000" X-Mailer: IncrediMail (6395248) From: "Frederick Moreno" X-FID: FLAVOR00-NONE-0000-0000-000000000000 X-Priority: 3 To: "Lancair Mail (lml@lancaironline.net)" Subject: Fw: RE: [LML] Changed subject to Gap Seals --------------Boundary-00=_C7K5SBX3LVC000000000 Content-Type: Multipart/Alternative; boundary="------------Boundary-00=_C7K5NM13LVC000000000" --------------Boundary-00=_C7K5NM13LVC000000000 Content-Type: Text/Plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable I put on glider gap seals and now 250 hours later, most are still in plac= e.=20 My approach: sanded the area where the adhesive hits the paint with 1500 sand paper after having wiped with acetone, heat gun to drive out residua= l acetone that may have remained, putting down masking tape to prevent sand= ing out of bounds, and then after applying tapes, repeated passes pushing dow= n hard with my thumbs - time and pressure being assumed necessary to make t= he adhesive flow into the tiny scratches. Not perfect, but seems to last better than experience of others.=0D =0D As for their effect, I assume small potatoes, but it all adds up. =0D =0D Fred =0D =0D =0D =0D =0D -------Original Message-------=0D =0D From: bronnenmeier@GROBSYSTEMS.COM=0D Date: 9/06/2013 12:27:06 AM=0D To: lml@lancaironline.net=0D Subject: RE: [LML] Changed subject to Gap Seals=0D =0D Danny,=0D =0D I buy my gap seals from =93wings and Wheels=94 =96 they have also picture= s and sketches on their site of how to mount them. My ex co-workers from GROB aircraft used their services (only for the gliders) for many years and we= re happy with them.=0D =0D Gap seals in general: I saw a speed increase may be of 2 kts at the most = =96 it is something that I question if I would do it again. I can=92t take th= em off again because when I removed old tape the paint came off on some spot= s.=0D =0D On my 4P gap seals have a very limited life time. I lose one about every = 15 =96 20 hrs of flight. No big deal =96 no safety hazard =96 it is just gon= e after the flight. I pay attention now that on decent I keep the airspeed from going into the yellow (200kts) too far. If I fool around with the airplan= e eg. taking dives until I hit red line (270kts) , flying over the runway f= ull throttle and pulling it straight up=85.. I can almost bet that one seal i= s missing.=0D =0D I pay really good attention that all the surfaces are clean and free of o= ld glue, I apply high pressure when initially applying the tape, I tried to = use a heat gun, I rough the surface of the mylar (usually the double sided ta= pe is still on the wing), I make sure that the inner tapes are still there a= nd sealed. In short: I am a person that works usually very detailed and I pu= t a lot of effort in applying the seals but I can=92t get them to stay on for good=85..=0D =0D In my opinion these seals are made for lower speeds than what we see in o= ur planes. If someone can give me some ideas of what other products / procedures to use I would be very happy=85.=0D =0D These are just my thoughts and there might be a better solution out there= =2E=0D =0D Ralf=0D =0D From: Sky2high@aol.com [mailto:Sky2high@aol.com] =0D Sent: Friday, June 07, 2013 12:52 PM=0D To: lml@lancaironline.net=0D Subject: Re: [LML] Changed subject to Gap Seals=0D =0D Do an internet search for "glider gap seals" as a start.=0D =0D Grayhawk=0D =0D In a message dated 6/7/2013 9:43:17 A.M. Central Daylight Time, danny@n10= 7sd com writes:=0D Speaking of gap seals, any recommendations on where to get them, how to attach them, whether to put them on a painted surface or sand it down?=0D =0D =0D Danny=0D LNC2-360 Mk-II=0D Nothing is foolproof to the sufficiently talented fool.=0D =0D =0D =0D From: Sky2high@aol.com [mailto:Sky2high@aol.com] =0D Sent: Friday, June 07, 2013 9:41 AM=0D To: lml@lancaironline.net=0D Subject: [LML] Re: VORTEX GENERATORS=0D =0D Chris,=0D =0D Dittos. Didn't Bob Belshe say he eventually retained the vortex generato= r only forward of the ailerons with better low speed control with them and less reduction in cruise speed. If ya add gap seals ya can get the cruis= e speed back and even increase control surface aukthority..............=0D =0D Grayhawk=0D =0D In a message dated 6/7/2013 7:12:09 A.M. Central Daylight Time, chris_zavatson@yahoo.com writes:=0D Being somewhat interested in aircraft efficiency, two quotes from the VG website jumped out at me.=0D =0D On the Lancair page: =0D " A 10 knot reduction in the stall speed; much better low speed handling = and no reduction in the cruise speed." =0D Then on the FAQ page:=0D " At maximum power, you may experience a 0-4 mph reduction, but this depe= nds on the particular aircraft. At normal cruising speed there is no noticeab= le reduction. "=0D =0D For me maximum power typically is cruise power. The speed loss will tend= to be on the higher side in a low drag airframe.=0D =0D VGs locally energize the boundary layer to keep the flow attached. This takes energy. Unfortunately a nice laminar flow section is turned into a partially turbulent flow wing. Everything is a trade-off.=0D =0D A previous link on the LML to Bob Belshe's 235 VG mod also reported a reduction in cruise speed of a couple knots.=0D =0D Here is another link to a flight test report of a Bonanza with a VG upgra= de.=0D http://www.nar-associates.com/technical-flying/vortex/Vgs_cruise_wide_scr= een pdf =0D =0D Chris Zavatson=0D N91CZ=0D 360std=0D www.N91CZ.net=0D =0D Sent from my spiffy iPad=0D =0D On Jun 4, 2013, at 3:55 AM, Rob Murawski wrote:=0D Nice info on the VG's! I've been contemplating whether to install the extended wingtips on my 360 MkII, now it looks like I have another option= to reduce the stall speed. Assuming I even need that.=0D =0D This doesn't make the decision-making process any easier.=0D =0D -Rob=0D Lancair 360MkII=0D 15% Complete=0D Pittsburgh, PA=0D =0D From: PETER WILLIAMS =0D Reply-To: Lancair Mailing List =0D Date: Tuesday, June 4, 2013 7:42 AM=0D To: =0D Subject: [LML] VORTEX GENERATORS=0D =0D HI THERE=0D =0D here is the link for vortex generator kits for Lancair aircraft=0D =0D http://www.pnwaero.com/Lancair.htm=0D =0D i was very happy with the company and with the results=0D =0D peter williams=0D =3D=0D =20 --------------Boundary-00=_C7K5NM13LVC000000000 Content-Type: Text/HTML; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
I put on glider gap seals and now 250 hours later, most are still in= place.  My approach: sanded the area where the adhesive hits the pa= int with 1500 sand paper after having wiped with acetone, heat gun to dri= ve out residual acetone that may have remained, putting down masking tape= to prevent sanding out of bounds, and then after applying tapes, repeate= d passes pushing down hard with my thumbs - time and pressure being assum= ed necessary to make the adhesive flow into the  tiny scratches.&nbs= p; Not perfect, but seems to last better than experience of others.
 
As for their effect, I assume small potatoes, but it all adds up.
 
Fred 
 
 
 
 
-= ------Original Message-------
 
From: bronnenmeier@GROBSYSTEMS.COM
Date: 9/06/2013 12= :27:06 AM
Subject: RE: [LML]= Changed subject to Gap Seals
 

Danny,

 

I buy my gap seals from =93wings and Whe= els=94 =96 they have also pictures and sketches on their site of how to m= ount them. My ex co-workers from GROB aircraft used their services (only = for the gliders) for many years and were happy with them.

 

Gap seals in general: I saw a speed incr= ease may be of 2 kts at the most =96 it is something that I question if I= would do it again. I can=92t take them off again because when I removed = old tape the paint came off on some spots.

 

On my 4P gap seals have a very limited l= ife time. I lose one about every 15 =96 20 hrs of flight. No big deal =96= no safety hazard =96 it is just gone after the flight. I pay attention n= ow that on decent I keep the airspeed from going into the yellow (200kts)= too far. If I fool around with the airplane eg. taking dives until I hit= red line (270kts) , flying over the runway full throttle and pulling it = straight up=85.. I can almost bet that one seal is missing.

 

I pay really good attention that all the= surfaces are clean and free of old glue, I apply high pressure when init= ially applying the tape, I tried to use a heat gun, I rough the surface o= f the mylar (usually the double sided tape is still on the wing), I make = sure that the inner tapes are still there and sealed. In short: I am a pe= rson that works usually very detailed and I put a lot of effort in applyi= ng the seals but I can=92t get them to stay on for good=85..

 

In my opinion these seals are made for l= ower speeds than what we see in our planes. If someone can give me some i= deas of what other products / procedures to use I would be very happy=85.=

 

These are just my thoughts and there mig= ht be a better solution out there.

 

Ralf

 

From: Sky2high@aol.com [mailto:Sky2high@aol.com]=
Sent: Friday, June 07, 2013 12:52 PM
To: lml@lancai= ronline.net
Subject: Re: [LML] Changed subject to Gap Seals

 

Do an internet search for "glider gap s= eals" as a start.

 

Grayhawk

 

In a message dated 6/7/2013 9:43:17 A.M. Cen= tral Daylight Time, danny@n107sd.com<= /A> writes:

Speaking of gap seals, any recom= mendations on where to get them, how to attach them, whether to put them = on a painted surface or sand it down?

 

 

Danny

LNC2-360 Mk-II=

Nothing is foolproof to the suff= iciently talented fool.

 

 

 

From: Sky2high@aol.com [mail= to:Sky2high@aol.com]
Sent: Friday, June 07, 2013 9:41 AMTo: lml@lancaironline.n= et
Subject: [LML] Re: VORTEX GENERATORS

 

Chris,

 

Dittos.  Didn't Bob Belshe say he eventually retai= ned the vortex generator only forward of the ailerons with better low spe= ed control with them and less reduction in cruise speed.  If ya add = gap seals ya can get the cruise speed back and even increase control surf= ace aukthority..............

 

Grayhawk

 

In a message dated 6/7/2013 7:12:09 A.M. Central Daylig= ht Time, chris_zavatson@yahoo.com writes:

Being somewhat interested in aircraft efficiency, two q= uotes from the VG website jumped out at me.

 

On the Lancair page: <= /SPAN>

" A 10 knot reduction in= the stall speed; much better low speed handling and no reduction = in the cruise speed."

Then on the FAQ page:<= /SPAN>

" At maximum power, you may experience a 0-4 mp= h reduction, but this depends on the particular aircraft. At nor= mal cruising speed there is no noticeable reduction. "

 

For me maximum power typically is cruise power. =  The speed loss will tend to be on the higher side in a low drag air= frame.

 

VGs locally energize the boundary layer to keep the flo= w attached.  This takes energy. Unfortunately a nice laminar flow se= ction is turned into a partially turbulent flow wing. Everything is a tra= de-off.

 

A previous link on the LML to Bob Belshe's 235 VG mod a= lso reported a reduction in cruise speed of a couple knots.

 

Here is another link to a flight test report of a Bonan= za with a VG upgrade.

http://www.nar-associates.com/technical-flying/vortex/Vgs_cruis= e_wide_screen.pdf


Chris Zavatson

N91CZ

360std


Sent from my spiffy iPad


On Jun 4, 2013, at 3:55 AM, Rob Murawski <rob@robmura= wski.com> wrote:

Nice info on the VG's!  I've been contemplating wh= ether to install the extended wingtips on my 360 MkII, now it looks like = I have another option to reduce the stall speed.  Assuming I even ne= ed that.

 

This doesn't make the decision-making process any easie= r.

 

-Rob

Lancair 360MkII

15% Complete

Pittsburgh, PA

 

From: PETER WILLIAMS <peterpawaviation@hotmail.com>
Reply-To: L= ancair Mailing List <lml@lancaironline.net>
Date: Tuesday, June 4, 2013 7:42 AM
To: <lml@lancaironline.= net>
Subject: [LML] VORTEX GENERATORS<= /P>

 

HI THERE

here is the link for vortex generator k= its for Lancair aircraft

http:/= /www.pnwaero.com/Lancair.htm

i was very happy with the company= and with the results

peter williams

=3D

 
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