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Relative loading on biplane wings
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.
System:
The UNT Digital Library