Computation of Coupled Unsteady Gas Flow Compressor/Turbine Rotational Dynamics in a High By-Pass-Ratio Three-Shaft Turbofan
46th AIAA Aerospace Sciences Meeting and Exhibit
01.01.2008
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2008
|Unsteady Flow Computation in a Double-Stage Double-Shaft Turbine
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|The Rolls-Royce Three Shaft Turbofan Engine
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|The Rolls-Royce three-shaft turbofan engine
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