34th Congress of the International Council of the Aeronautical Sciences

05 - Propulsion

AERODYNAMIC DEFORMATION EXPERIMENT OF SERPENTINE NOZZLE FOR TURBOFAN AND ANALYSIS OF FLUID-STRUCTURE INTERACTION METHOD

Q.-L. Li¹, L. Zhou¹, Z.-X. Wang¹, X.-B. Zhang¹, S. Huang¹; ¹Northwestern Polytechnical University, China

In this paper, an experimental study on structural deformation of serpentine nozzle for turbofan engine is carried out?and the reliability of one-way/two-way fluid-structure coupled was verified. The deformation is mainly located in the second bend channel, and the two-way fluid-structure coupled method can more accurately simulate the aerodynamic deformation characteristics of the nozzle.


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