NASA NTRS · 19930092097
A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow
Abstract
A compilation of theoretical values of the lateral-stability derivatives for wings at supersonic speeds is presented in the form of design charts. The wing plan forms for which this compilation has been prepared include a rectangular, two trapezoidal, two triangular, a fully-tapered swept-back, a sweptback hexagonal, an unswept hexagonal, and a notched triangular plan form. A full set of results, that is, values for all nine of the lateral-stability derivatives for wings, was available for the first six of these plan forms only. The reasons for the incompleteness of the results available for other plan forms are discussed.
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Jones, Arthur L, Alksne, Alberta. 1951-01-01. A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow. https://ntrs.nasa.gov/citations/19930092097
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