Return-Path: Received: from [24.25.9.102] (HELO ms-smtp-03-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.2b3) with ESMTP id 87896 for flyrotary@lancaironline.net; Mon, 24 May 2004 17:19:21 -0400 Received: from EDWARD (clt25-78-058.carolina.rr.com [24.25.78.58]) by ms-smtp-03-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id i4OLJGLr015339 for ; Mon, 24 May 2004 17:19:17 -0400 (EDT) Message-ID: <000c01c441d4$c9840080$2402a8c0@EDWARD> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Shielding material selection Date: Mon, 24 May 2004 17:19:23 -0400 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1409 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1409 X-Virus-Scanned: Symantec AntiVirus Scan Engine Thanks, Alex Great to have your research/knowledge on the topic. Now I know why the aluminum foil seemed to work so well. Ed Anderson > > > > David, your observation was correct on the temperature of aircraft. > > However white paint would make be a bad shielding for the inside of a > > cowl. > > Here is what I got from my heat transfer book: > > > > A=solar absorptivity > > E=infrared emissivity & absorptivity > > > > Surface A E > > AL polished .09 .03 > > AL foil .15 .05 > > > > Stainless Steel Polished .37 .6 > > SS Dull .5 .21 > > > > Black Paint .97 .97 > > Wight Paint .14 .93 > > > > > > These numbers are very interesting. For shielding we want the lowest E. > > For trying to block radiant heat AL is clearly the best. Stainless steel > > is between 4 and 12 times worse at blocking radiation that AL foil. > > > > Trying to keep objects cool under sunlight is a special case. We want it > > to have a low A so that it does not absorb much solar energy but a high > > E so that it easily radiates any acquired energy away. Note white paint > > is great for this. > > > > The bottom line is that white paint is great for solar shielding on the > > outside of but bad for infrared shielding under cowlings and such. Al is > > the best for IR shielding. > > > > > > I am missing all the Greek letters so a am kind of mangling the > > radiation formula but here it is. > > Qrad= a*G*A + a*E*O(Tinf^4-Tsurf^4) > > > > Qrad=heat transfer (W/M^2) > > a=area of surface (M^2) > > G=solar radiation (W/M^2) > > A= solar absorptivity > > E= infrared emissivity > > O=5.67E-8 (W/(M^2*K^4) > > Tinf= temperature of the surroundings (K) > > Tsur= Temperature of the surface (K) > > > > NOTE temperatures must be in Kelvin > > > > > > Alex Madsen > > > > > > > > > > > > > > -----Original Message----- > > From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On > > Behalf Of Alex Madsen > > Sent: Monday, May 24, 2004 1:28 AM > > To: Rotary motors in aircraft > > Subject: [FlyRotary] Re: Two problems solved, 2 more pop up... > > > > I am skeptical of this. Where the light colored aircraft composite? This > > would make a difference. The higher thermal conductivity of the AL would > > make it seem much hotter than composites. Both aircraft must be > > constructed of the same material. Were they? Anyway off to look at my > > heat transfer book to see what it has to say on this topic. > > > > Alex Madsen > > > > -----Original Message----- > > From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On > > Behalf Of David Carter > > Sent: Sunday, May 23, 2004 11:49 PM > > To: Rotary motors in aircraft > > Subject: [FlyRotary] Re: Two problems solved, 2 more pop up... > > > > I've noticed that shiney polished aluminum airplanes are quite hot in > > the > > sun, whereas white and light cream colored painted exteriors are quite > > cool. > > I used to think and "aluminum" finish would be best for reflecting heat, > > but > > I no longer think that. I think the same situation would prevail inside > > the > > cowl. > > > > David > > > > ----- Original Message ----- > > From: "Chad Robinson" > > To: "Rotary motors in aircraft" > > Sent: Sunday, May 23, 2004 9:25 PM > > Subject: [FlyRotary] Re: Two problems solved, 2 more pop up... > > > > > > Given that the primary goal is reflecting radiated heat (rather > > than > > "real" > > > thermal insulation) what's wrong with a coat or two of shiny silver > > paint? > > > It's not as good as polished aluminum but it's decent, and high on the > > > reflective scale. Sherwin Williams (and others) sells a product called > > > "Silver-Brite" that is marketed as "heat reflective" and "dry heat > > resistant > > > to 700degF". I haven't tested its adherence to epoxy so it might need > > a > > primer > > > coat to help it stick better (it's designed for metal) but that's not > > a > > > painful step. In any event, it would sure be a lot easier to apply > > than > > either > > > foil OR fiberfrax, especially to an oddly-shaped cowl. > > > > > > Unless real thermal insulation properties are necesary? > > > > > > Regards, > > > Chad > > > > > > > > >> Homepage: http://www.flyrotary.com/ > > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > > > > >> Homepage: http://www.flyrotary.com/ > > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > > > > >> Homepage: http://www.flyrotary.com/ > > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html