Development Testing of the RB.211 Turbofan Engine
1970; Emerald Publishing Limited; Volume: 42; Issue: 11 Linguagem: Inglês
10.1108/eb034695
ISSN2059-9366
Tópico(s)Rocket and propulsion systems research
ResumoTHE 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.
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