NASA NTRS · 19930090800
Approximation method for determining the static stability of a monoplane glider
Abstract
The calculations in this paper afford an approximate solution of the static stability. A derivation of the formulas for moment coefficient of a wing, moment coefficient of elevator, and the total moment of the combined wing and elevator and the moment coefficient with reference to the center of gravity are provided.
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Lippisch, A. 1927-11-01. Approximation method for determining the static stability of a monoplane glider. https://ntrs.nasa.gov/citations/19930090800
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