Computation of Coupled Unsteady Gas Flow Compressor/Turbine Rotational Dynamics in a High By-Pass-Ratio Three-Shaft Turbofan
46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV
01.01.2008
15 pages
Aufsatz (Konferenz)
Englisch
Aeronautics , Astronautics , AIAA , Aerospace
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