Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Sun, 08 Aug 2004 23:50:20 -0400 Message-ID: X-Original-Return-Path: Received: from out011.verizon.net ([206.46.170.135] verified) by logan.com (CommuniGate Pro SMTP 4.2) with ESMTP id 357379 for lml@lancaironline.net; Sun, 08 Aug 2004 23:04:23 -0400 Received-SPF: pass receiver=logan.com; client-ip=206.46.170.135; envelope-from=res0ic5s@verizon.net Received: from HalsPC ([4.47.49.59]) by out011.verizon.net (InterMail vM.5.01.06.06 201-253-122-130-106-20030910) with ESMTP id <20040809030351.SKJO14580.out011.verizon.net@HalsPC> for ; Sun, 8 Aug 2004 22:03:51 -0500 From: "Hal Woodruff" X-Original-To: "'Lancair Mailing List'" Subject: L-IV glide ratio X-Original-Date: Sun, 8 Aug 2004 20:03:39 -0700 X-Original-Message-ID: <000001c47dbd$7c8023c0$0300a8c0@HalsPC> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.2627 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 X-Authentication-Info: Submitted using SMTP AUTH at out011.verizon.net from [4.47.49.59] at Sun, 8 Aug 2004 22:03:40 -0500 I took Dan Schaefer's advice and went out over the weekend to test the glide ratio for my IV=P. I'm satisfied now that the best glide happens at about the same numbers reported in the IV's operations manual. I found in my data quite a bit of data scatter but the trend was there and L/D max occurred at approx. 115 knots. Correcting for the weight I was flying to gross weight would put the best glide a little less than 120 kts. The best L/D computed to 8:1. I did most of the testing with the throttle pulled all the way back to idle with the assumption that the best glide speed would be the same speed regardless of whether the engine was idling or off. For my last glide I pulled the mixture to lean cutoff with the expectation of increased descent speed. Interestingly, I couldn't discern any noticeable change in the descent rate. Quite frankly, I couldn't discern any change in engine noise either. The only way I could tell that the engine wasn't still running was the fuel flow went to zero. The oil pressure remained in the low 40's and was sufficient to enable the prop to be pulled to full coarse pitch. The change in descent rate was amazing - to the tune of about 40% reduction in descent. The L/D ratio computed to 11:1 with the prop in this configuration. As Dan suggested, this test is something that everyone should do to "characterize" the performance of their particular airplane. BTW, when I pulled the mixture to idle-cutoff, I had a 10,000 foot runway 7000 feet beneath me. Hal Woodruff IV-P