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    In:  CASI
    Publication Date: 2019-06-28
    Description: Recent improvements in stress analysis methods have made it necessary to revise and to extend the loading curves to cover all conditions of flight. This report is concerned with a study of existing biplane data by combining the experimental and theoretical data to derive a series of curves from which the lift curves of the individual wings of a biplane may be obtained.
    Type: NACA-TR-458
    Format: application/pdf
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