Relative loading on biplane wings
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.
Date:
February 15, 1933
Creator:
Diehl, Walter S.
Item Type:
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Partner:
UNT Libraries Government Documents Department