Return-Path: Sender: (Marvin Kaye) To: lml Date: Wed, 06 Nov 2002 19:45:12 -0500 Message-ID: X-Original-Return-Path: Received: from JSC-EMS-VWS04.jsc.nasa.gov ([139.169.39.51] verified) by logan.com (CommuniGate Pro SMTP 4.0) with SMTP id 1854809 for lml@lancaironline.net; Wed, 06 Nov 2002 17:44:24 -0500 Received: from 139.169.16.60 by JSC-EMS-VWS04.jsc.nasa.gov (InterScan E-Mail VirusWall NT); Wed, 06 Nov 2002 16:43:08 -0600 Received: by jsc-smtp02.jsc.nasa.gov with Internet Mail Service (5.5.2653.19) id ; Wed, 6 Nov 2002 16:43:08 -0600 X-Original-Message-ID: <1848CABD3587A84DAC6B3F82FE01D9FC01F1FC0C@jsc-mail08.jsc.nasa.gov> From: "THORN, VALIN B. (JSC-OM) (NASA)" X-Original-To: "'lml@lancaironline.net'" Subject: RE: [LML] LNC2 Tail Incidence, Rudder Cables X-Original-Date: Wed, 6 Nov 2002 16:43:08 -0600 MIME-Version: 1.0 X-Mailer: Internet Mail Service (5.5.2653.19) Content-Type: text/plain Re: [How about this? Figure out (calculate) the difference in pitching moment caused by the heavier engine... Rob Wolf ] Yea Rob, I just may do that. I've even been tempted to build a full performance analysis model for the Legacy, eventually. Has anyone out there already done that? Anyway, I still need to get an idea of how good Lancair's original design calculations were since they had to be guessing at the pitching moment of the fuselage during design. Even if I calculate an accurate delta AOI, I may be starting from one that's already non-optimal. Hopefully someone flying an IO-550 Legacy has taken some in flight pictures that show the elevator trim position (from another airplane or out the back window) or they've set up their control stick so that it shows the angle their controls are at... (hmmmm, that might be cool...) Thanks, Valin Legacy 173 BTW, in case anyone has tried to send an email to our home address lately, our host's server has been down for several days now. Just send to work email in the mean time. Thanks.