X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 23 Apr 2014 12:01:04 -0400 Message-ID: X-Original-Return-Path: Received: from nm38-vm1.bullet.mail.bf1.yahoo.com ([72.30.239.17] verified) by logan.com (CommuniGate Pro SMTP 6.0.9e) with ESMTPS id 6842887 for lml@lancaironline.net; Tue, 22 Apr 2014 16:14:48 -0400 Received-SPF: pass receiver=logan.com; client-ip=72.30.239.17; envelope-from=chris_zavatson@yahoo.com Received: from [98.139.212.150] by nm38.bullet.mail.bf1.yahoo.com with NNFMP; 22 Apr 2014 20:14:14 -0000 Received: from [98.139.212.243] by tm7.bullet.mail.bf1.yahoo.com with NNFMP; 22 Apr 2014 20:14:14 -0000 Received: from [127.0.0.1] by omp1052.mail.bf1.yahoo.com with NNFMP; 22 Apr 2014 20:14:14 -0000 X-Yahoo-Newman-Property: ymail-3 X-Yahoo-Newman-Id: 347550.24753.bm@omp1052.mail.bf1.yahoo.com Received: (qmail 70642 invoked by uid 60001); 22 Apr 2014 20:14:14 -0000 DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; h=X-YMail-OSG:Received:X-Rocket-MIMEInfo:X-Mailer:Message-ID:Date:From:Reply-To:Subject:To:MIME-Version:Content-Type; b=vttxOJ36kbQI9BcididINyAWkk05hRL8YkSo/PMImTkqm9zlQxfE9glUixwFoZxAJKXRun7c6ZnKLxUt6QS9awU+A/4gV9lddOh/cBZ6Rv/dTjjLy8OmY0qaVHYJElqrrcHP0G/z9AWw4Sg8H4/99OnwGCPOIOoXyNxTts9mgMQ=; X-YMail-OSG: HCE44IkVM1ng1xFz5SBuOYmMMHS8mv3kOIltkbj6fdWvTE0 8hw.E0MZ1CXxPFHNv.I.myaaNMYaIzn6Wl4A8dqBzjDFffK7AiA08qzcGtPx ux_g9CKBhnRYsKo5w7qk.WM7BT1D4ijckWNjqmzExpDjIUEGnPmhm734kM2U dwW0pLmtXLwzRM1IVD8eDGihqNDngURXOJwb9SkMEeqref.zm.25Y2oSeUmz vAztVBQC1Wm4FRq_H7Yk_.1jCkTQFq7cEV92TO806u9ngAlmsgvgTMsee07l 9SGHJy.0hBDhsMbxPS3i7qjCd.UlO0orTZFgHIL2hcCV9bhG.bD4eaYgu_jv 8axIlHy0EMCarWsQ8bT46_NA3AJeYLCRpVcbkiHXmD1Lb_sb2j7Jt4bUJlHu 5mqnlYVZhAvVFXvbYlngnyQqveSnKoeoVjLxo1lKMNhLmymFflmewfHM.O7i MMb4DYMkNBRHT5Zs2dPyEpV5ReuJdAo_o6b1VmFYnUyKeuSNo9cz.T9VcWQ7 Ja4Lsr_CFiW1GGC9GOd13mfXKqJcd7SFS9dL30lfYDqGxX7VloOmvy60- Received: from [172.14.16.72] by web161202.mail.bf1.yahoo.com via HTTP; Tue, 22 Apr 2014 13:14:14 PDT X-Rocket-MIMEInfo: 002.001,PT09PT09PT09PT09PT09PT09CkNocmlzLAoKRXhjZWxsZW50IEFuYWx5c2lzLgoKU2luY2UgdGhlIDMyMCBoYXMgZ290IHRvIGJlIHRoZSBtb3N0IGluZGl2aWR1YWxseSBtb2RpZmllZCBraXQgcGxhbmUsIGNvdWxkICB5b3UgYmUgbW9yZSBzcGVjaWZpYyBhYm91dCBkZXRhaWxzIG9mwqB0aGUgZWxldmF0b3Igc3lzdGVtIGluIHRoZSAzMjAgdXNlZCAgZm9yIGNvbXBhcmlzb246CgoxLiBXYXMgdGhlIGVsZXZhdG9yIGJlbGwgY3JhbmsgYXJtIDQiIChvcmlnaW5hbCBkZXNpZ24pIG9yIDMiIChwb3B1bGFyIG0BMAEBAQE- X-Mailer: YahooMailWebService/0.8.185.657 X-Original-Message-ID: <1398197654.32138.YahooMailNeo@web161202.mail.bf1.yahoo.com> X-Original-Date: Tue, 22 Apr 2014 13:14:14 -0700 (PDT) From: Chris Zavatson Reply-To: Chris Zavatson Subject: Large/small tail stability comparison X-Original-To: LML posts MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="356309654-511931412-1398197654=:32138" --356309654-511931412-1398197654=:32138 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=0AChris,=0A=0AExcell= ent Analysis.=0A=0ASince the 320 has got to be the most individually modifi= ed kit plane, could you be more specific about details of=A0the elevator s= ystem in the 320 used for comparison:=0A=0A1. Was the elevator bell crank = arm 4" (original design) or 3" (popular mod) as this affects stick forces = and movement distances?=0A=0A2.=A0Since the spring trim system was used, wa= s=A0the trim the=A0original crucifix and spring=A0system or was=A0the=A0Re= ichel trim wheel with stronger springs used?.=A0 This has some effect on t= rim rigidity and stick forces for elevator movement away from the trimmed = position.=A0 You did mention that trim tabs could alter certain results (e= ven the tab sizes used by builders may be quite different).=0A=0A3. Was th= e bob weight installed?=A0 Recently some builders claimed=A0that they did= =A0not install the bob weight that was designed to increase stick forces u= nder increased aircraft=A0loading.=0A=0AConsidering these variables, what i= mplications might they have with respect to observations/conclusions made = in=A0your report?=0A=0AThanks,=0A=0AScott Krueger=0A=3D=3D=3D=3D=3D=3D=3D= =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=0A=0AScott,=0AGood observations.= =0A1. Shortened. I will add that detail along with stick travel per elevato= r travel.=0A2.=A0 Reichel trim wheel.=A0 I am trying to line=A0up=A0an abbr= eviated=A0test on a small tail 360 that uses an electric trim tab to evalua= te the influence of the spring.=0A3. Yes, bob weight installed, will add th= at as well.=0A=0AStick fixed stability is not affected by any of the above.= =A0 It looks at rigid elevator position regardless of how it is achieved.= =A0 Stick free response may be influenced by the spring, in particular, whe= n getting farther off the trim point.=A0 For example the phugoid that=A0bec= ame somewhat violent.=A0 Initial thoughts are that=A0the spring=A0could be = negatively influencing the low speed end where hinge moments start dropping= off rapidly.=A0=A0I hope to have some data on that soon.=0AChris=0A --356309654-511931412-1398197654=:32138 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
=3D=3D=3D=3D=3D= =3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D
Chris,
 
Excellent Analysis.
 
Since the 320 has g= ot to be the most individually modified kit plane, could you be more speci= fic about details of the elevator system in the 320 used for comparis= on:
 
1. Was the elevator bell crank arm 4" (origi= nal design) or 3" (popular mod) as this affects stick forces and movement = distances?
 
2. Since the spring trim system = was used, was the trim the original crucifix and spring sys= tem or was the Reichel trim wheel with stronger springs used?.&n= bsp; This has some effect on trim rigidity and stick forces for elevator m= ovement away from the trimmed position.  You did mention that trim ta= bs could alter certain results (even the tab sizes used by builders may be quite different).
&= nbsp;
3. Was the bob weight installed?  Recently some builde= rs claimed that they did not install the bob weight that was des= igned to increase stick forces under increased aircraft loading.
 
Considering these variables, what implications might= they have with respect to observations/conclusions made in your repo= rt?
 
Thanks,
 
Scott Kru= eger
=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D=3D= =3D

Scott,
Good observations.
= 1. Shortened. I will add that detail along with stick travel per elevator t= ravel.
2.  Reichel trim wheel.  I am trying to line&nbs= p;up an abbreviated test on a small tail 360 that uses an electri= c trim tab to evaluate the influence of the spring.
3. Yes, bob w= eight installed, will add that as well.

Stick fixed stability is not affected by an= y of the above.  It looks at rigid elevator position regardless of how= it is achieved.  Stick free response may be influenced by the spring,= in particular, when getting farther off the trim point.  For example = the phugoid that became somewhat violent.  Initial thoughts are t= hat the spring could be negatively influencing the low speed end = where hinge moments start dropping off rapidly.  I hope to have s= ome data on that soon.
Chris

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