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    A study of the pitching moments and the stability characteristics of monoplanes (1934)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: 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.
    Type: NACA-TN-511
    Format: application/pdf
    Location Call Number Expected Availability
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