Development of the Tilt-Wing Aircraft-Reference-Cited by-同舟云学术

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Development of the Tilt-Wing Aircraft

Published:1963-06 Issue:630 Volume:67 Page:361-370
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Nichols John B.

Abstract

The author accepted the invitation to present this paper on the rash assumption that he would be able to present something new and useful on the tilt-wing. The Hiller Company (in partnership with Vought and Ryan) was the first to have received a fully-fledged development contract for evaluation quantities of any VTOL machine. The VHR-447 which was selected as the Army, Navy and Air Force XC-142A was a culmination of almost ten years of effort spent in the investigation and promotion of the tilt-wing “propello-plane” VTOL aircraft concept.

Publisher

Cambridge University Press (CUP)

Reference24 articles.

1. Stuart Joseph III . Propeller Lifted Tilt Wing VTOL Aircraft. Aero Engineering Review, August 1956.

2. Templin R. J. Note on the Minimum Power Required for Flight at Low Airspeeds. Canadian National Research Laboratories Report LR245, May 1959.

3. Guerrieri M. and Stuart J. III . A Simplified Theoretical Investigation of a Wing Propeller Combination Through a Range of Angles-of-Attack from 0° to 90° and a Comparison With Experimental Results. Hiller Report No. 461·3, 14th October 1955.

4. Geddes Phillip . The VTOL Transport—Design Selection. Aircraft and Missiles, April 1960.

5. McKinney M. O. Jr. What Price VTOL? Space Aeronautics, May 1959.

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