X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=PNVxBsiC c=1 sm=1 tr=0 a=heuW58uY1yy9w+pfVyFuFQ==:117 a=jpOVt7BSZ2e4Z31A5e1TngXxSK0=:19 a=x7bEGLp0ZPQA:10 a=xXDCcK6TKBsA:10 a=FmdZ9Uzk2mMA:10 a=pGLkceISAAAA:8 a=Ia-xEzejAAAA:8 a=UTAyDOTzzI0fxlg1xSsA:9 a=tiMajCt31gQmZoil:21 a=WezNUqMLSYPCgjVb:21 a=QEXdDO2ut3YA:10 a=mNizCT58O9tLcwBlukcA:9 a=dbTHNZuide49Zn67:21 a=AaaC0wv-dtle0xnU:21 a=x7ZpgCcNBALD-3Gc:21 a=Urk15JJjZg1Xo0ryW_k8:22 From: "Todd Bartrim bartrim@gmail.com" Received: from mail-ed1-f51.google.com ([209.85.208.51] verified) by logan.com (CommuniGate Pro SMTP 6.2.13) with ESMTPS id 12862838 for flyrotary@lancaironline.net; Tue, 20 Aug 2019 18:31:30 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.208.51; envelope-from=bartrim@gmail.com Received: by mail-ed1-f51.google.com with SMTP id p28so562820edi.3 for ; Tue, 20 Aug 2019 15:31:31 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=mime-version:references:in-reply-to:from:date:message-id:subject:to; bh=tri0tM6ZFLbzbckEdBRQk7IjZHY9JfmM7KXBzHze2WM=; b=F8sybWutUxDM4Q8dZlCtgX4VmpYuGHyqGOYFVj7oicG/Xi8S5DuNGiEWDo3UCMaLJi fmwTg1yhUSj2OQ26ojPYCakbkcJ/Y6hL2QjuxDCY3tkgijKlcqM3Hjg7P71qyCzvI/At UO7yjmBv9TonuJq8/UYaECVnofdKib5fmNLcD3yksJfj/s+Uza93bcRlt6EKjuFpg0WR NNuKLS3KALp511sK7J19g+f9PM+VftBjxhMecacYthcMJVa2rZ9V6NfJXmuYRO6aTL0l RJDXWvfbtuofeZn6xA797wJlrBqQG132SDC92Al2iUlkL2RTgmZcgFtaFiFKQgl+W8Js 3Hgg== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:mime-version:references:in-reply-to:from:date :message-id:subject:to; bh=tri0tM6ZFLbzbckEdBRQk7IjZHY9JfmM7KXBzHze2WM=; b=qjMZZek6YIfsEVzxTylBK/+jgs7Y/blVN5+A2680xkIlmQnsTi30bNhppdEQg8lFz9 wGFF3TGCuiD8DrP+gKZTu/iWeVzRn00ztoDHRwyQQUMwzjfXlo6oQbCGXeXKY0BLGnci p+Gf3Ytr7Q//MGztBRucdAREWKUuvbWwDn7W+PLBF80OLUqJXIQeAJA7mf67/dCZ7Ugm 3AvqDP3r22qtEO48l2al/EMu4d/TPy6GZysenOGvek2U3VMpaMt7qZAqOyztVOELRgjq 3SkYDXFz6ncWOzDQpNARYmkmwJRJlF5uVihpM2gTB0hDXvacIcryx8Tcm+1Pru12KebC umMA== X-Gm-Message-State: APjAAAVNvYslO/W8LTyRwWbQ+vpSBSycLU34Wp8CB9TamFn7C+4xfl0A X/eP1STp8gUeyysK70zY4+UOMa6nQMTqIi9qL1ot X-Google-Smtp-Source: APXvYqynjW9DXjmfeAWHG2KjVzcCNQijQtYZFR2djuEhuFKcISxkKCH7Jj63fBucN28u1JfxL40UdZ8Hvza+CJFtOp0= X-Received: by 2002:a50:ace2:: with SMTP id x89mr33227180edc.268.1566340273029; Tue, 20 Aug 2019 15:31:13 -0700 (PDT) MIME-Version: 1.0 References: In-Reply-To: Date: Tue, 20 Aug 2019 15:31:00 -0700 Message-ID: Subject: Re: [FlyRotary] Re: airflow characteristics-radiators and spinner To: Rotary motors in aircraft Content-Type: multipart/alternative; boundary="0000000000009246bc05909403e4" --0000000000009246bc05909403e4 Content-Type: text/plain; charset="UTF-8" Hi Bill; Sorry to be resurrecting such an old email thread, but ever since you made this post, I've been thinking abut these rads. The possibilities are interesting. Do you have any other possible info on this model or any other suitable rads? I searched hi and low for dimensions of this rad, then found one on ebay that was photographed on a sheet of peg board which allows for a good estimation of size. It appears to be approx 12"x14" core and with the tanks being wedge shaped, it looks like it may just be an ideal fit to put 2 of these under an RV cowl. My concerns would be; first is it appears to only be approx 1.5" thick. Next is how thick is the aluminum on the tanks? I'm not a bad TIG welder, but I have my limits as to how thin I can reliably weld. And I would have to change the plumbing a little. And what kind of pressures are they designed for? I use a 20psi cap on my system. I'm considering ordering one off ebay that's only $40, just to check fitment, however they want $50 for shipping. Up here there are more snowmobile salvage shops than motorcycle... Todd Bartrim C-FSTB On Tue, Jul 9, 2019 at 2:24 PM William Jepson wrjjrs@gmail.com < flyrotary@lancaironline.net> wrote: > Group something else to note is that even in the P51 duct later models had > a wing section to help direct the airflow into the top section of the duct. > The idea has always been to slow the airflow to take advantage of whatever > fin pitch is used and then to pinch the duct again to re-speed the > airstream to near to the aircraft speed. Never 100% obviously but as close > to it as possible. Now I going to pass along a possibility for cooling that > I have told a few people but not many. There are a bunch of conformal > radiators available to us for a reasonable cost that I am amazed nobody is > using. High-performance motorcycle radiators. I worked for Kawasaki years > ago and did a lot of engine building even into the water-cooled era. > Several motorcycle manufacturers have built beautiful curved aluminum > radiators to increase the cooling available on some of their highest > performance models. I have attached a jpeg of the radiator from a Kawasaki > ZX7R. 750cc engine rated at about 110 HP. Very high heat rejection > requirements. Lots of these components available from motorcycle salvage > yards. often with minor damage to the end tanks, but for our use we might > modify them anyway. Fitting one, (or two), of these curved radiators inside > a cowl would be easyand effective. You might never get a radiator man to > make you a ring radiator, but you can buy some that might conform very well > to an in-cowl mounting. > Bill Jepson > > > --0000000000009246bc05909403e4 Content-Type: text/html; charset="UTF-8" Content-Transfer-Encoding: quoted-printable
Hi Bill;
=C2=A0 Sorry to be resurrect= ing such an old email thread, but ever since you made this post, I've b= een thinking abut these rads. The possibilities are interesting. Do you hav= e any other possible info on this model or any other suitable rads?=C2=A0
I searched hi and low for dimensions of this rad, then found one o= n ebay that was photographed on a sheet of peg board which allows for a goo= d estimation of size. It appears to be approx 12"x14" core and wi= th the tanks being wedge shaped, it looks like it may just be an ideal fit = to put 2 of these under an RV cowl.=C2=A0
My concerns would be; f= irst is it appears to only be approx 1.5" thick. Next is how thick is = the aluminum on the tanks? I'm not a bad TIG welder, but I have my limi= ts as to how thin I can reliably weld. And I would have to change the plumb= ing a little.
And what kind of pressures are they designed for? I= use a 20psi cap on my system.
I'm considering ordering one o= ff ebay that's only $40, just to check fitment, however they want $50 f= or shipping.
Up here there are more snowmobile salvage shops than= motorcycle...

Todd Ba= rtrim
C-FSTB


On Tue, Jul 9, 2019 at 2:= 24 PM William Jepson wrjjrs@gmail.com <flyrotary@lancaironli= ne.net> wrote:
Group something else to note is that even in the P51= duct later models had a wing section to help direct the airflow into the t= op section of the duct. The idea has always been to slow the airflow to tak= e advantage of whatever fin pitch is used and then to pinch the duct again = to re-speed the airstream to near to the aircraft speed. Never 100% obvious= ly but as close to it as possible. Now I going to pass along a possibility = for cooling that I have told a few people but not many. There are a bunch o= f conformal radiators available to us for a reasonable cost that I am amaze= d nobody is using. High-performance motorcycle radiators. I worked for Kawa= saki years ago and did a lot of engine building even into the water-cooled = era. Several motorcycle manufacturers have built beautiful curved aluminum = radiators to increase the cooling available on some of their=C2=A0 highest = performance models. I have attached a jpeg of the radiator from a Kawasaki = ZX7R. 750cc engine rated at about 110 HP. Very high heat rejection requirem= ents. Lots of these components available from motorcycle salvage yards. oft= en with minor damage to the end tanks, but for our use we might modify them= anyway. Fitting one, (or two), of these curved radiators inside a cowl wou= ld be easyand effective. You might never get a radiator man to make you a r= ing radiator, but you can buy some that might conform very well to an in-co= wl mounting.
Bill Jepson


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