Tilt Wing Aircraft in comparison with other VTOL and STOL Systems

Author:

Stepniewski W Z

Abstract

The CHAIRMAN, in introducing the Author, said that although it had in the past been the main concern of the Association to discuss the problems of the conventional helicopter, it was now proposed to include systems allied to it, and convertiplanes and other powered lift systems would be considered at this and future meetings of the Association There was now a whole spectrum of proposed direct lift aircraft ranging from the conventional helicopter of a few pounds per sq ft disc loading, to jet lift aircraft of hundreds of pounds per sq ft of jet area Between these two extremes there was a variety of convertiplanes and jet wing systemsThe Author had been working on rotorcraft for a long time He had been Chief Aerodynamicist of the Vertol Aircraft Corporation and Director of Aeronautical Research there, he had written many papers relating to the helicopter especially on aerodynamics, and his books on the subject published by the Rotorcraft Publishing Committee had been very widely read, even on this side of the Atlantic

Publisher

Cambridge University Press (CUP)

Reference12 articles.

1. Draper, J W and Kuhn, R E “Investigation of the Aerodynamic Characteristics of a Model Wing-Propeller Combination and of the Wing and Propeller Separately at Angles of Attack up to 90°,” NACA Rep 1263, 1956

2. Kirby, R H “Stability and Control of Propeller-Driven Transport VTOL Aircraft,” Proceedings of the XIII Annual National Forum, American Helicopter Society, 1957

3. Zimmerman, C H “Some Stability Problems of Vertically Rising Aircraft,” Proceedings of the Second Annual Western Forum, American Helicopter Society, 1955

4. Stepniewski, W Z “A Comparison Between Pay-Load Capabilities of VTOL and Conventional Aircraft,” Engineering Review, August, 1956

5. Stepniewski, W Z and Mallen, Joseph “Evaluation of VTOL Systems Suitable for Transport Applications,” Aeronautical Engineering Review, September, 1957

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