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A study of the pitching moments and the stability characteristics of monoplanesThis 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.
Document ID
19930081302
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Higgins, George J (Aeronautical Engineering Department, University of Michigan)
Date Acquired
September 6, 2013
Publication Date
November 1, 1934
Report/Patent Number
NACA-TN-511
Report Number: NACA-TN-511
Accession Number
93R10592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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