Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Fri, 14 Nov 2003 12:19:10 -0500 Message-ID: X-Original-Return-Path: Received: from mta5.adelphia.net ([68.168.78.187] verified) by logan.com (CommuniGate Pro SMTP 4.1.6) with ESMTP id 2731645 for lml@lancaironline.net; Fri, 14 Nov 2003 10:17:49 -0500 Received: from worldwinds ([68.169.129.81]) by mta5.adelphia.net (InterMail vM.5.01.06.05 201-253-122-130-105-20030824) with SMTP id <20031114151751.SKOA11705.mta5.adelphia.net@worldwinds> for ; Fri, 14 Nov 2003 10:17:51 -0500 From: "Gary Casey" X-Original-To: "lancair list" Subject: kinetic energy X-Original-Date: Fri, 14 Nov 2003 07:17:47 -0800 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 Importance: Normal <> Okay, I can't stop myself - got to jump in. Pounds "weight" is actually a force, pounds "mass" is a convenience term that is the mass of an object that exerts 1 pound of force on a scale at a standard gravity. We engineers commonly use the shortcut of talking about lbm (pounds mass). The term "slug" is defined as the mass for which one lbf will accelerated it at one ft/sec^2. The commonly accepted acceleration of "standard gravity" (at 45 degrees latitude) is 32.174 ft/sec^2 and hence a slug is about 32.2 lbm, not 31.25. All that doesn't mean anything much, so let's compute the temperature of the brake rotor after a maximum-energy stop. For a 3400 lbm aircraft stopping from 80 kts the kinetic energy to be absorbed by the brakes is almost 474,000 ft-lb, or 609 BTU's (some, but not a lot of energy is absorbed by aerodynamic drag and tire losses, while the residual thrust is working the other way). I don't know what a brake rotor weighs, but I'll guess 5 pounds. One thing I couldn't find is the specific heat of cast iron, but most steel alloys have a specific heat of between 0.1 and 0.14, so I'll pick 0.12. The temperature rise during a braking event is then BTU/(sp.ht.Xlbm), or about 1,000 degrees F. The brake temperature at the beginning could be 100, but if you drag the brakes a lot during taxi, heating them up to maybe 500 and then do a rejected takeoff, you could see 1500 degrees. The brake pad material will probably continue to work at 1,000 degrees, but probably not at 1,500. You might think that some of the heat gets absorbed in the caliper and wheel, but it is not so - almost all the heat goes directly into the rotor and very little is rejected into the air during that short time. Metallic linings will keep working at higher temperatures than conventional organics so that would help. Gary Casey