Helicopter Design: Some Elementary Considerations on Efficiency and Control
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1942
Abstract
REPORTS from America speak of flight tests of two types of screw‐lift aircraft, the Sikorsky multi‐rotor machine, and a twin‐rotor type. From this it would seem that the day of the practical helicopter, so Ions foreshadowed, is not far distant. The following general notes on design considerations may therefore be sufficiently topical to be of interest.
Citation
Lockwood Taylor, J. (1942), "Helicopter Design: Some Elementary Considerations on Efficiency and Control", Aircraft Engineering and Aerospace Technology, Vol. 14 No. 1, pp. 18-18. https://doi.org/10.1108/eb030862
Publisher
:MCB UP Ltd
Copyright © 1942, MCB UP Limited