Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 10 Dec 2002 00:32:19 -0500 Message-ID: X-Original-Return-Path: Received: from mailnw.centurytel.net ([209.206.160.237] verified) by logan.com (CommuniGate Pro SMTP 4.0.2) with ESMTP id 1898546 for lml@lancaironline.net; Mon, 09 Dec 2002 23:13:41 -0500 Received: from c656256a (pppoe-64-91-103-77.rb.gh.centurytel.net [64.91.103.77] (may be forged)) by mailnw.centurytel.net (8.12.6/8.12.6) with SMTP id gBA4DdPq007652 for ; Mon, 9 Dec 2002 20:13:40 -0800 (PST) X-Original-Message-ID: <009301c29ffa$e6201da0$0100a8c0@mshome.net> From: "Robert Smiley" X-Original-To: "Lancair Mailing List" References: Subject: Re: [LML] AILERON WEIGHT X-Original-Date: Mon, 9 Dec 2002 20:19:04 -0700 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_008E_01C29FC0.38500260" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 5.50.4133.2400 X-MimeOLE: Produced By Microsoft MimeOLE V5.50.4133.2400 This is a multi-part message in MIME format. ------=_NextPart_000_008E_01C29FC0.38500260 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Gary, Good question in my mind also. I used the chord line of the aileron and = adjusted weight so the chord line was horizontal. Now the wing tip = washes in compared to the wing stub but it may still have some positive = attack with respect to the relative wind in normal flight. If the = ailerons were not attached to the controls the aileron TE would probably = be above the flap and wingtip TE. =20 Bob Smiley N94RJ ------=_NextPart_000_008E_01C29FC0.38500260 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Gary,
 
Good question in my mind also. I used the chord = line of=20 the aileron and adjusted weight so the chord line = was horizontal.  Now=20 the wing tip washes in compared to the wing stub but it may still have = some=20 positive attack with respect to the relative wind in normal flight. If = the=20 ailerons were not attached to the controls the aileron TE would probably = be=20 above the flap and wingtip TE. 
 
Bob Smiley
N94RJ
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