Return-Path: Received: from slkcpop1.slkc.uswest.net ([206.81.128.1]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with SMTP id com for ; Fri, 12 Mar 1999 09:53:37 -0500 Received: (qmail 28747 invoked by alias); 12 Mar 1999 14:55:33 -0000 Received: (qmail 28734 invoked by uid 0); 12 Mar 1999 14:55:33 -0000 Received: from edsl164.slkc.uswest.net (HELO scottdah.slkc.uswest.net) (209.181.81.164) by pop.slkc.uswest.net with SMTP; 12 Mar 1999 14:55:33 -0000 Delivered-To: fixup-lancair.list@olsusa.com@fixme From: "Scott Dahlgren" To: "___Lancair list" Subject: NASA duct Date: Fri, 12 Mar 1999 07:57:37 -0700 Message-ID: Importance: Normal X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> the NASA duct used on the 320 was designed originally from nasa with a rounded lip on the end of the duct. A rounded lip could be hinged to limit the air volume without creating extra drag (that is what I am hoping to do). I will post the article on NASA ducts from EAA's sport aviation to marv with all the drawings if anyone wants them. I am also interested in the shocks. let me know what the volume price is and the weight if anyone knows it. thanks, Scott