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Development Testing of the RB.211 Turbofan Engine: An account of the test programme for the development of the RB.211 advanced technology turbofan for the Lockheed L‐1011 airliner

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1970

Abstract

THE Rolls‐Royce RB.211 advanced technology turbofan for the Lockheed L‐1011 TriStar has been designed from the outset for case of maintenance by the embodiment of modular construction and development testing at Hucknall and Derby is confirming the inherent advantages of its three‐shaft layout for large high bypass ratio propulsion systems.

Citation

(1970), "Development Testing of the RB.211 Turbofan Engine: An account of the test programme for the development of the RB.211 advanced technology turbofan for the Lockheed L‐1011 airliner", Aircraft Engineering and Aerospace Technology, Vol. 42 No. 11, pp. 28-31. https://doi.org/10.1108/eb034695

Publisher

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MCB UP Ltd

Copyright © 1970, MCB UP Limited