Add a section for camber.
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@ -88,6 +88,9 @@ wing: This defines the main wing of the aircraft. You can have
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constrained well by the solution process, and may
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require tuning to get throttle settings correct in
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high AoA (approach) situations.
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camber: The lift produced by the wing at zero angle of
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attack, expressed as a fraction of the maximum
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lift produced at the stall AoA.
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hstab: These defines the horizontal stabilizer of the aircraft.
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Internally, it is just awing objects and therefore work the
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