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This calculator is based on the TAIL VOLUME (TVo) work done by WIlliam McCombs and Don DeLoach. HERE is the link to the Don DeLoach article. Input your measured |
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The CG Values are to be applied to the AVERAGE WING CHORD, as calculated. Wing and Tail Areas can be calculated in a variety of ways. Straight rectangular wings are simple span multiplied by chord. Wings with straight tapered sections can be calculated by applying additional trangular formulae. Wings with curved sections are difficult to measure without a CAD program. |