NASA Technical Reports Server (NTRS) 19930090735: Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing

Book details

Title
NASA Technical Reports Server (NTRS) 19930090735: Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing
Publication year listed
1926
Format
Public domain eBook
Reading access
Free online reader; no registration required
Source record
View on Archive.org

About this book

NASA Technical Reports Server (NTRS) 19930090735: Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing

Author: NASA Technical Reports Server (NTRS)

Year: 1926

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.

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