Return-Path: Received: from www06.netaddress.usa.net ([204.68.24.26]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with SMTP id com for ; Wed, 30 Dec 1998 21:25:58 -0500 Received: (qmail 10676 invoked by uid 60001); 31 Dec 1998 02:27:19 -0000 Message-ID: <19981231022719.10675.qmail@www06.netaddress.usa.net> Date: Thu, 31 Dec 1998 02:27:19 From: Dan Schaefer To: lancair.list@olsusa.com Subject: reflexing and flaperons X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Thanks, Scott, for the interesting comments about reflexing. I don't know what airfoil Lancair used on the 320/360 models, though I believe (rightly or wrongly, to be sure) that they all used *essentially* the same wing with the same NLF series profile. Just prior to buying my 235 kit, back in '85-'86, I researched the airfoils that Lance used (the information was available, either in his literature or in a magazine article) by contacting the folks at NASA - at Langley, if I remember correctly (CRS due to age, they tell me) - as I had heard a lot of wind tunnel data had been generated on this series of foils, and they made their data available through a friend. Two features stand out in the data (and I'm sorry, but I loaned the package out many years ago and it never came back): When in the laminar flow regime, the airfoil has better drag numbers, that is, lower, than the turbulent flow shapes in common use today; second, and the one that I thought was most impressive, if the laminar flow is tripped such that it goes turbulent (due to rain or bug accumulation maybe), it does not experience a large loss of lift - just higher drag (nice if you run through a patch of rain on short final); and third, what you pay for all this good stuff, quite a bit higher than "normal" (that is, compared to commonly used airfoils) pitching moment. All wings want to turn nose down when they are producing lift (well, all that I know about) and the NLF series just want to do it with a lot more force. One thing that impressed the importance of reflexing to relieve the stresses set up in the wing by the high pitching moment was the factory pilot who checked me out in my airplane (Mike DeHate) being VERY insistant about going to full reflex at and above 160 MPH IAS. When the factory guy speaks, I listen (particularly when it was his butt up there with me). Later, Dan Schaefer