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  • 1
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    Unknown
    The calculation of lateral stability with free controls (1934)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The discussion of the structural methods for obtaining lateral stability discloses the remarkable influence of the constant fuselage and wing proportions to the yawing moments. For the effectiveness of modifications in vertical tail surfaces and tail length, these quotas - little observed heretofore, in this connection - are decisive. This also applies to the amount of dihedral of the wing with regard to the roll stability of the complete wing already existing without angle of the dihedral.
    Type: NACA-TM-741
    Format: application/pdf
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