| To: | <land-speed@Autox.Team.Net> |
|---|---|
| Subject: | Re: Streamliner question. |
| From: | "John Burk" <joyseydevil@comcast.net> |
| Date: | Wed, 1 Dec 2004 17:01:16 -0500 |
My copy of Theory of Wing Sections shows short fat NACA basic thickness forms (streamlined shapes) with up to 15 deg per side convergent angles - The drag goes up some as the angle increases but form drag is a small part of a streamliners total aero drag . |
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