Wake studies of eight models propellers /

Analysis of previous force tests in the light of wake characteristics reveals that, for constant-speed operation, pitch should be so distributed that no element will operate at a negative lift coefficient in high-speed flight, that shank stalling during take-off and climb will be minimized, and that...

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Bibliographic Details
Main Author: Reid, Elliott G
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington D.C. : National Advisory Committee for Aeronautics, 1946
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1040; 1040, Suppl
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Stanford University

Holdings details from Stanford University
Call Number: NACA TN 1040
NACA TN 1040:SUPPL.