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A Further Development in Calculating the Takeoff to 50 ft. Distance of an Aeroplane

A Further Development in Calculating the Takeoff to 50 ft. Distance of an Aeroplane A SERIES of laborious calculations of takeoff distance indicated the desirability of expressing propeller thrust as a function of speed in the takeoff range so that the ground run could be integrated directly. Propeller thrusts were estimated from REF. 2 for a wide range of disk loadings, solidities, and tip speeds. Plotting against speed shows that, for practical values, the assumption of linearity introduces a negligible error see FIGS. 739. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

A Further Development in Calculating the Takeoff to 50 ft. Distance of an Aeroplane

Aircraft Engineering and Aerospace Technology , Volume 20 (4): 4 – Apr 1, 1948

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb031621
Publisher site
See Article on Publisher Site

Abstract

A SERIES of laborious calculations of takeoff distance indicated the desirability of expressing propeller thrust as a function of speed in the takeoff range so that the ground run could be integrated directly. Propeller thrusts were estimated from REF. 2 for a wide range of disk loadings, solidities, and tip speeds. Plotting against speed shows that, for practical values, the assumption of linearity introduces a negligible error see FIGS. 739.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Apr 1, 1948

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