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Author Topic: How do you find the wing area in sq in?  (Read 1093 times)

Offline Paul Taylor

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How do you find the wing area in sq in?
« on: August 05, 2009, 09:00:00 PM »
OK --- I am going to try and do some math. n~

How do I find the wing area... and are the flaps included?
Paul
AMA 842917

As my coach and mentor Jim Lynch use to say every time we flew together - “We are making memories

Offline Scott Hartford

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Re: How do you find the wing area in sq in?
« Reply #1 on: August 05, 2009, 09:23:14 PM »
It's usually printed on the front of the box or on the plans.... LL~





Don't shoot!, Just making a funny...... ;D

Offline Ralph Wenzel (d)

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Re: How do you find the wing area in sq in?
« Reply #2 on: August 05, 2009, 09:34:44 PM »
Flaps are included, as is the area masked by the fuselage. For a straight taper wing, add the root and tip chords and multiply by ˝ the total span.

For elliptical or semi-elliptical wings, multiply the root chord times the full span x ⅔ (This is not exact, but is an excellent approximation).

(Too many irons; not enough fire)

Ralph Wenzel
AMA 495785 League City, TX

Offline Louis Rankin

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Re: How do you find the wing area in sq in?
« Reply #3 on: August 06, 2009, 09:14:23 AM »
Paul,

Wing Length (span) measured in inches multiplied by wing width (cord) measured in inches will usually yield an accurate measurment of square inches.

If wing is taperd, as mentioned above, you need to find your Mean Average Cord (MAC) by adding root and tip cord together and then dividing by 2.

For wing loading: Divide wing area in square inches by 144 to obtain square feet.  Then divide weight in ounces by squre feet to obtain wing loading in ounces per square foot.

Example: Typical model of 550 wing area and 44 ounces of weight.  To find sq. ft. 550/144 = 3.8194.  To find wing loading 44/3.8194 = 11.5201

There is much debate over the best target wing loading; however, Jim Lynch has told me many times "Do not build under 10 and do not go over 14 ounces of wing loading.
Louis Rankin
Somerville Tennessee
AMA 10859


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