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Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing

Authors :
Wolff, E B
Koning, C
Publication Year :
1926
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1926.

Abstract

Experiments were performed with a wing model, to which a rotary cylinder had been fitted. The rotation of the cylinder had a remarkable effect on the aerodynamic properties of the wing.

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19930090735
Document Type :
Report

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