Return-Path: Received: from burgoyne.com ([209.197.0.8]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 16 Feb 1999 16:49:17 -0500 Received: from clkeller.burgoyne.com (sl6.burgoyne.com [209.197.0.45]) by burgoyne.com (8.9.1/8.9.1) with SMTP id OAA29797 for ; Tue, 16 Feb 1999 14:50:58 -0700 Message-ID: <36C9E285.1CC7@burgoyne.com> Date: Tue, 16 Feb 1999 14:26:29 -0700 From: "C.L.Keller" To: lancair.list@olsusa.com Subject: Aerodynamic Data X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Can anyone provide a source for (1) aerodynamic data on the airfoil used on the 320/360, supposedly the NLF-0215-F, and (2) design data and analysis of NACA air inlet scoops. Charles Keller. [Charles... You might want visit the NASA website (http://www.nasa.gov) and use their search engine on the terms "submerged-duct", "submerged-inlet", "NACA flush", and whatever else you might think of with related terminology, and I'm sure you'll find more documents than you'll know what to do with about NACA ducts. There is a new link on my Links page to an airfoil analysis program which has recently come available, or you can get there directly by using the following link: http://www.bawel.net/~airfanalysis/. I would imagine that the data on the L320 airfoil is probably included in the standard data set which accompanies the software. I hope this helps. ]