>
> Hi Paul and group,
>
> An engineer, from Texas related to the NexusMustang Yahoo groop, has
> sent me this link.  It is not related to rotary
> engine.  But I would
> like to share this link with all of you.
>
> http://www.bicambertechnology.com/
>
> Marc Joseph
>
> That has been around for years. Airfoils are VERY VERY easy to test
> for lift to drag ratio performance. If it was any good Boeing would
> be using it.
>
> Where are the lift to drag ratio curves? The web site is all BS.
> A waste of your time.
>
> Buy this cheap book and you will know as much as anyone knows
> about wings.
> http://www.amazon.com/Theory-Wing-Sections-Including-
> Summary/dp/0486605868
> Paul Lamar

The book is in the mail.  Thanks Paul :))

Marc Joseph

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