A study of the pitching moments and the stability characteristics of monoplanes

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Summary: This note presents a study of the pitching moments and the stability characteristics of monoplanes. Expressions for the pitching-moment coefficient and the Diehl stability coefficient for the monoplane are developed, suitable for the use of airplane designers. The effective difference between the high-wing and low-wing types is portrayed and discussed. Comparisons between experimental and computed values are made. Charts for use in the solution of numerical values of the pitching-moment and stability coefficients are presented.
Collection: NASA Technical Reports Server (NTRS) Collection.
Note: Document ID: 19930081302.
Accession ID: 93R10592.
NACA-TN-511.
Terms of Use and Reproduction: No Copyright.

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