Unsymmetrical lift distributions on a stalled monoplane wing

Unsymmetrical lift distributions on a stalled monoplane wing

The purpose of the research was to find if it is possible to have an unsymmetrical span load distribution on a monoplane wing at the stall without a rolling velocity. The investigation is based upon the Prandtl first order wing theory. It is shown that it is possible to have an unsymmetrical lift...

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Bibliographic Details
Main Author: Schairer, Robert Sorg
Format: Others
Published: 1939
Online Access:https://thesis.library.caltech.edu/5153/1/Schairer_r_1939.pdf
Schairer, Robert Sorg (1939) Unsymmetrical lift distributions on a stalled monoplane wing. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/3WX9-JZ33. https://resolver.caltech.edu/CaltechETD:etd-12282005-110200 <https://resolver.caltech.edu/CaltechETD:etd-12282005-110200>

Internet

https://thesis.library.caltech.edu/5153/1/Schairer_r_1939.pdf
Schairer, Robert Sorg (1939) Unsymmetrical lift distributions on a stalled monoplane wing. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/3WX9-JZ33. https://resolver.caltech.edu/CaltechETD:etd-12282005-110200 <https://resolver.caltech.edu/CaltechETD:etd-12282005-110200>

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