Can you limit the max speed by prop pitch and still retain phenoninal
climb characteristics with lots of hp?





> Ameet:
>
>  Thanks for setting me straight on the terminology.  What I used for wing
> area is exactly what you sdescribe as I used  36 inches x 94 inches  for
> the outbboard wings on mine to run through the theoretical stall speed
> calcs to arrive at max allowable gross for the 51 mph stallof 887#  for my
> bird.
>
> I am depending on engine & Prop choice as well as the drag of the Tri-gear
> to get the speed under the 138 mph limit.  I would of course love the
> "Pocket Rocket" status afforded by some of the larger engine sizes.
>
> Don
>
> Ameet Savant wrote:
>
>> Eric - The airfoil and hence the curvature neither the
>> thickness of it has any bearing on the wing area for
>> aerodynamic calculations. In other words, simply
>> calculate the area of the polygon traced by the wing
>> to get the wing area.
>>
>> Don - MAC is a weighted average of all cord lengths on
>> a semi-span. This is useful for simplifing aerodynamic
>> calculations on a tapered wing. MAC is same as chord
>> on a rectangular wing.
>>
>> Ameet Savant
>> Omaha, NE
>>
>> --- D F Lively <[email protected]> wrote:
>>
>> > Eric:
>> >
>> > I can be wrong on this but I think that is whaht is
>> > ment by the MACwhich is the
>> > lingthof the line 1l2 way between the upper and
>> > lower surface which would be
>> > slightly longer.  I would not worry about the
>> > theoretical benifits of that
>> > though because as a practical mater there are
>> > probably enough imperfections
>> > elsewhere to eat up what little is gained by
>> > cosidering the difference.
>> >
>> > Don
>> >
>> >
>> ----------------------------------------------------------------
>> >
>> > Eric Anderson wrote:
>> >
>> > > I read somewhere that the square footage of a wing
>> > is what you would get if
>> > > if you stripped the upper surface off and laid it
>> > out flat. So it is always
>> > > a little more than the chord x span.
>> > >
>> > > -Eric in Mpls
>>
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