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Approximation method for determining the static stability of a monoplane gliderThe 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.
Document ID
19930090800
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lippisch, A
Date Acquired
September 6, 2013
Publication Date
November 1, 1927
Report/Patent Number
NACA-TM-436
Report Number: NACA-TM-436
Accession Number
93R20090
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - GLIDERS
GLIDERS - STABILITY, STATIC-GLIDERS
GLIDERS - DES

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