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Powered Lift Systems

Published online by Cambridge University Press:  26 October 2023

Charles H Zimmerman
Charles H Zimmerman*
Affiliation:
National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory, Langley Field, Va, U S A

Extract

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The CHAIRMAN, in opening the meeting, said that Mr Zimmerman, a member of the scientific staff of the National Advisory Committee for Aeronautics, at Langley Field, Virginia, had long been concerned with the development of S T O L aircraft, having originated and developed the Chance-Vought circular-wing project during the war at Stratford, Connecticut In the rotary wing field, he was perhaps best known as the originator of the Flying Platform, having designed and built at Nicholls, Connecticut, shortly after the war, his so-called “Aerial Motor-cycle,” which had two side-by-side lifting propellers of disc loading about 20, interconnected by a tiny platform which he strapped to his feet like skis By 1947, he was able to demonstrate to his satisfaction that this device required no controls other than a throttle for the two engines, and that he could hover safely by applying the same reactions to his feet as he used for balancing himself when standing on the ground

Type
Research Article
Information
The Journal of the Helicopter Association of Great Britain , Volume 12 , Issue 4 , August 1958 , pp. 141 - 159
Copyright
Copyright © Royal Aeronautical Society 1958

References

1 McKinney, M O NACA Research on VTOL and STOL Airplanes Paper presented to Anglo-American Aeronautical Conference of the Royal Aeronautical Society and Institute of the Aeronautical Sciences, Sept 2—15, 1957Google Scholar
2 Kuhn, R E, and Draper, J W Investigation of Effectiveness of Large-Chord Slotted Flaps in Deflecting Propeller Slipstreams Downward for Vertical Take-off and Low-Speed Flight NACA TN 3364, January, 1955Google Scholar
3 Kuhn, R E Take-off and Landing Distance and Power Requirements of Propeller-Driven STOL Airplanes Preprint No 690, Institute of the Aeronautical Sciences, January, 1957Google Scholar
4 McKinney, M O, Kuhn, R E, and Hammack, J B Problems in the Design of Propeller-Driven Vertical Take-off Transport Airplanes Aeronautical Engineering Review, Vol 15, No 4, April, 1956, pp 68—75, 84Google Scholar
5 Zimmerman, Charles H NACA Research in the Field of VTOL and STOL Aircraft Preprint No 814, Institute of the Aeronautical Sciences, January, 1958Google Scholar
6 Schubauer, G B Jet Propulsion With Special Reference to Thrust Augmenters NACA TN 442, January, 1933Google Scholar
7 Lowry, J G, Riebe, J M, and Campbell, J P The Jet-Augmented Flap Preprint No 715, S M F Fund Preprint, Institute of the Aeronautical Sciences, January, 1957Google Scholar
8 Vogler, Raymond D, and Turner, Thomas R Wind-Tunnel Investigation at Low Speeds to Determine Flow-Field Characteristics and Ground Influence on a Model With Jet-Augmented Flaps NACA TN 4116, September, 1957Google Scholar
9 Campbell, John P, and Johnson, Joseph L Jr, Wind-Tunnel Investigation of an External-Flow Jet-Augmented Flap Suitable for Application to Airplanes With Pod-Mounted Jet Engines NACA TN 3898, December, 1956Google Scholar
10 Davenport, Edwin E Wind-Tunnel Investigation of External-Flow Jet-Augmented Double-Slotted Flaps on a Rectangular Wing at an Angle of Attack of 0° to High Momentum Coefficients NACA TN 4079, September, 1957Google Scholar