ABCDEFGHIJKLMNOPQRSTUVWXYZ
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Spreadsheet for calculating basic lift paramaters
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from Sport Aviation
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JGR 11/89
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H (altitude)0rho (density)0.00237689
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V (knots)24V (ft/sec)40.536
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W (weight)500V (mph)27.648
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KNOWNSOLVE FOR
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CL (lif coeff)2.3S (wing area)111.3220763
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KNOWNSOLVE FOR
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S (wing area)110CL (lift coeff)2.327643414
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KNOWNSOLVE FOR
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S (wing area)110V (knots)28.94739416
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CL (lift coeff)1.6
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3.055555556931.3333333
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