X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail-vc0-f174.google.com ([209.85.220.174] verified) by logan.com (CommuniGate Pro SMTP 6.0.1) with ESMTPS id 6092298 for flyrotary@lancaironline.net; Sat, 02 Mar 2013 13:29:19 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.85.220.174; envelope-from=thomasmann51@gmail.com Received: by mail-vc0-f174.google.com with SMTP id n11so2657565vch.33 for ; Sat, 02 Mar 2013 10:28:43 -0800 (PST) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20120113; h=mime-version:x-received:in-reply-to:references:date:message-id :subject:from:to:content-type; bh=A7lgs/5wrDwCG72lST3/AJeObx7DTZlQGS/SFPMXgnI=; b=Vu8QFG6peD6gmE6/cWMryfXcCMFruwlydERm0gKuWLyuKihMPJBcBXwVnT996XrRBt 3+svA9lq/qwNi8L5Rl0RP/KfR+Lzw5y+Lvlx6VVltUXCCAHzjcwN5lW44ehN5VJ7wVQ2 n9C8U2cBpZpomXuTOv1/Ka2uVgrG3KjdQTLx/ECSVWbJLK791Q8XecLLxfM+qHJpR4BS pbZ/Z0C+DRlLOskarwyrSPCAfshXhSk+fTxQjHB8G45WEczsgBeO51hiVNsmglDaWo5y oD2MGpHrQmMWYUurq0BnBjP6DLZMOYznukoByeLt2ChZ/Ze+jbhLNXGTFBAFAPKaOYcO 9ODA== MIME-Version: 1.0 X-Received: by 10.52.23.18 with SMTP id i18mr4899662vdf.46.1362248923447; Sat, 02 Mar 2013 10:28:43 -0800 (PST) Received: by 10.58.75.75 with HTTP; Sat, 2 Mar 2013 10:28:43 -0800 (PST) In-Reply-To: References: Date: Sat, 2 Mar 2013 12:28:43 -0600 Message-ID: Subject: Re: [FlyRotary] P-51 type belly scoops From: Thomas Mann To: Rotary motors in aircraft Content-Type: multipart/alternative; boundary=20cf307ca5762d867a04d6f54b4c --20cf307ca5762d867a04d6f54b4c Content-Type: text/plain; charset=ISO-8859-1 The P-51 Scoop is how I plan on cooling my 20B (Long-EZ) I scaled down the drawings of the original P-51 plans in Auto CAD and fit it into my plan drawing and it looks as though it will make for a nice compact design. The original P-51 design splits the airfow sending a portion to the oil cooler and the rest to the radiator. Both have a controlable exhaust door to meter the airflow leaving the unit. The original P-51 has no thermostat. Temperature is regulated by the position of the exhaust door. On takeoff and landing the doors are wide open. The rest of the time they are automatically controlled to regulate the temperatures. I'm just about to the point where I will be flipping my bird on it's back in order to install the cooling system. The P-51 design (if done correctly) can create enough thrust to cancel out 90% of the drag caused by the scoop. --20cf307ca5762d867a04d6f54b4c Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable
The P-51 Scoop is how I plan on cooling my 20B (Long-EZ)
= =A0
I scaled down the drawings of the original P-51 plans in Auto= CAD and fit it into my plan drawing and it looks as though it will make fo= r a nice compact design.
=A0
The original P-51 design splits the airfow sending a por= tion to the oil cooler and the rest to the radiator. Both have a controlabl= e exhaust door to meter the airflow leaving the unit.
=A0
<= div> The original P-51 has no thermostat. Temperature is regulated by the positi= on of the exhaust door. On takeoff and landing the doors are wide open. The= rest of the time they are automatically controlled to regulate the tempera= tures.
=A0
I'm just about to the point where I will be flipping= my bird on it's back in order to install the cooling system.
=A0
The P-51 design (if done correctly) can create enough thrust= to cancel out 90% of the drag caused by the scoop.
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