[NSRCA-discussion] Wing Sweep Angle?

[J N Hiller]

Thanks Ron, but I can't imagine that the aerodynamic affect (dihedral) would
be the same for wings having different taper.
Jim

-----Original Message-----
From: nsrca-discussion-bounces at lists.nsrca.org
[mailto:nsrca-discussion-bounces at lists.nsrca.org]On Behalf Of Ronald Van
Putte
Sent: Sunday, December 08, 2013 3:21 PM
To: General pattern discussion
Subject: Re: [NSRCA-discussion] Wing Sweep Angle?

The wing leading edge.  That's what's important when approaching Mach 1 and
that's what aerodynamicists use.

Ron

On Dec 8, 2013, at 4:16 PM, J N Hiller wrote:

> Question!
> How dose one measure wing sweep angle on tapered wing panels? Is it
located
> as a percentage of cord?
> Jim Hiller
>
>
>
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