[NSRCA-discussion] Wing Sweep Angle?

[Ronald Van Putte]

Imagine what you want.

Ron

On Dec 8, 2013, at 6:35 PM, J N Hiller wrote:

> 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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