Tilt Wing Propelloplane Design Requirements

SM_WF_1956-4684

10/1/1956

Authors
Abstract
Content

Tilt wing propelloplanes are broadly described, The selections of propeller disk loadings and some of the significant differences between rotor and propeller lifted high performance aircraft are briefly discussed. Possible propelloplane control systems and their relative advantages are mentioned, Brief consideration is given to longitudinal balance and other practical design problems. Primary emphasis is given to a study of the unusual aerodynamic characteristics of tiltwing propelloplanes in the hovering and the accelerating and decelerating transition regimes of flight The decelerating transition from airplane type flight to hovering flight is shown to be the critical maneuver for propelloplanes.

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DOI
https://doi.org/10.4050/SM_WF_1956-4684
Citation
Stuart III, J., "Tilt Wing Propelloplane Design Requirements," Western Forum 1956, Dallas, Texas, October 1, 1956, https://doi.org/10.4050/SM_WF_1956-4684.
Additional Details
Publisher
Published
10/1/1956
Product Code
SM_WF_1956-4684
Content Type
Technical Paper
Language
English