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A leading Canadian engineering institution is offering a Ph.D. position focused on improving turbomachine efficiency through a comprehensive research program. The selected candidate will work on developing numerical strategies for blade/casing contact phenomena and will actively involve undergraduate students. Ideal candidates should have a strong background in vibrations, nonlinear dynamics, and programming in Python. The job starts on September 1, 2026, and offers a full-time temporary contract until January 30, 2026.
Organisation/Company École Polytechnique de Montréal Research Field Engineering Researcher Profile Recognised Researcher (R2) Leading Researcher (R4) First Stage Researcher (R1) Established Researcher (R3) Country Canada Application Deadline 30 Jan 2026 - 22:00 (UTC) Type of Contract Temporary Job Status Full-time Offer Starting Date 1 Sep 2026 Is the job funded through the EU Research Framework Programme? Not funded by a EU programme Is the Job related to staff position within a Research Infrastructure? No
Context and objectives
More stringent environmental constraints and a very competitive global context force manufacturers to face new challenges in order to improve the efficiency of turbomachines, be it in the aerospace sector or for power generation. The impossibility to compromise safety or the environmental footprint of such systems means that in early design stages designers must now understand and account for nonlinear vibration phenomena - such as blade/casing contacts - that are still only partially characterized today. The proposed Ph.D. project is part of a larger research program that aims at developing a numerical strategy for the simulation, the characterization and the consideration of blade/casing contact phenomena within compressor blade design stages using two complementary solution paradigms: in the time domain and in the frequency domain. This research program will give the opportunity to both industrial partners to share their common knowledge and expertise on this topic in order to develop a uniform numerical tool suited both for gas turbines blades and aircraft engine blades.
The proposed research has three main objectives:
Work environment
The selected candidate will be part of the LAVA which currently employ several researchers and graduate students working in areas closely related to that of the proposed research. All numerical developments will be made using the Python programming language. The candidate will benefit from the digital research infrastructure at LAVA (wiki website, gitlab platform, data and computation servers). The candidate will have the opportunity to supervise undergraduate students throughout the duration of the project.
The selected candidate will ideally have advanced notions of vibrations and nonlinear dynamics. A good knowledge of modelling methodologies including the finite element method is preferred. All numerical developments will be carried out using the Python programming language.