Continuation techniques for analysis of whole aeroengine dynamics with imperfect bifurcations and isolated solutions
Harmonic balance
Rubbing
Rotordynamics
Continuation
Numerical continuation
DOI:
10.1007/s11071-016-3003-y
Publication Date:
2016-08-10T15:59:13Z
AUTHORS (4)
ABSTRACT
The analysis of whole engine rotordynamic models is an important element in the design aerojet engines. include gyroscopic effects and allow for rubbing contact between rotor stator components such as bladed discs casing. Due to nonlinearities inherent system, bifurcations frequency response may arise. Reliable efficient methods determine bifurcation points solution branches are required. For this purpose, a multi-harmonic balance approach presented that allows numerically detection calculation both continuous isolated functions. method applied test case derived from commercial aeroengine. A structure with observed studied paper. comparison time marching based on simulations shows accuracy numerical efficiency newly developed approach.
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