Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Thu, 03 Jun 2004 19:16:32 -0400 Message-ID: X-Original-Return-Path: Received: from c60.cesmail.net ([216.154.195.49] verified) by logan.com (CommuniGate Pro SMTP 4.2b4) with ESMTP-TLS id 122917 for lml@lancaironline.net; Thu, 03 Jun 2004 19:04:47 -0400 Received: from unknown (192.168.1.40) by c60.cesmail.net with QMQP; 03 Jun 2004 19:04:15 -0400 Received: from 12.146.136.195 ([12.146.136.195]) by webmail.spamcop.net (Horde) with HTTP for ; Thu, 3 Jun 2004 16:04:15 -0700 X-Original-Message-ID: <20040603160415.lvwvc4cwcs4g4kow@webmail.spamcop.net> X-Original-Date: Thu, 3 Jun 2004 16:04:15 -0700 From: bob mackey X-Original-To: lml@lancaironline.net Subject: Re: Unsafe at any speed MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1" Content-Disposition: inline Content-Transfer-Encoding: 7bit User-Agent: Internet Messaging Program (IMP) 4.0-cvs Some people say Lancair IVs are inherently unsafe and people are crashing and dieing as a result. Some people say that Lancair IVs are the finest aircraft ever built and they crash only because the pilots or builders are not up to the task. You're both right, and you're both wrong. By the admission of many on this list, various models of Lancairs have agressive stall-spin characteristics. Adequate pilotage can avoid stalls and spins, but so can design changes. Those who insist that better training is required are correct as any pilot who dies in the plane clearly needed more training to deal with whatever deadly situation he found that day. Those who say that the airplane is unsafe are also correct -- the stall/spin characteristics could undoubtedly be tamed by modifications to the airframe. Larger tail, forward CG shift, stall strips, wing twist, airfoil modifications and so on are all common and well understood engineering approaches to the taming of nasty stall properties. Properly done, these changes would have little or no detrimental effect on the high speed cruise that we love, and would probably improve the low-speed handling. Those who say that the plane is safe and would only be crashed by bad piloting are wrong. There are clearly good pilots that are still managing to get in trouble. A more forgiving airframe might have kept them alive. Those who say that the airframe is unsafe and can't be flow safely are also mistaken. There are situations in which the pilot and the plane are up to the task and arrive at the destination swiftly and and proud to be flying in one of the best airplanes ever built. We are experimental aviators. We can make ourselves safer through pilot training, engineering, or both. If we do neither, then we earn our smoking craters. ---------------------- The segment of this discussion that has been lacking so far (IMO) is consideration of *how* to make the airframe safer. In my experience with the design of ultralight sailplanes, it is possible to design for extreme spin resistance while also maintaining high performance. One method that could be adapted here would be to change the aileron/flap mixing schedule. With the flaps down, I'm not too concerned with high-speed cruise. The wingtips could be made more spin resistant by allowing the ailerons to deflect up more as the flaps go down. This effectively increases twist, lowering the tip angle of attack. This in turn helps to prevent tip stall, and maintains aileron authority when the midwing begins to stall. Would this help? I don't know without testing. I would start with modelling in Mark Drela's Xfoil software, then build RC models with electronically controlled flap-aileron mixing, then build a full-size mechanical mixer for testing in life size. The testing with a human on board would require a skilled test pilot as well as a spin 'chute and/or whole-airframe parachute. How about some other suggestions for building safer Lancairs without giving up the performance that we love? - bob mackey flying a 235 building a 320 103MD -at- pure-flight.com [use this email address, the one at the top is spam bait]