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A Finite Step Method for the Calculation of Span Loadings of Unusual Plan Forms
Report presenting an investigation of the applicability of a finite-step method to the calculation of subsonic spanwise load distribution, lift-curve slope, lateral center of pressure, and aerodynamic center of unusual plan forms. The 20-step method was found to generally overestimate the amount of loading at the wing tip, but the lift-curve slope, lateral center of pressure, aerodynamic center, and loading shape generally agreed with lifting-surface results.
Date:
July 16, 1951
Creator:
Campbell, George S.
System:
The UNT Digital Library
Removal of ruptured slug from tube No. 1476-D
None
Date:
July 16, 1951
Creator:
Shadinger, C. D.
System:
The UNT Digital Library