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Master's Thesis Opportunity: Multi-Fidelity Propeller Optimization for Hybrid-Electric eVTOL Aircraft

Confidential company · Ottobrunn · Posted Sep 18, 2026

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Public summary

A Master's student is sought to conduct a six-month thesis project focused on developing a multi-fidelity propeller optimization framework for hybrid-electric eVTOL aircraft. The project involves extending existing automated design workflows to integrate low- and high-fidelity aerodynamic and aeroacoustic models, with collaboration between a university aerodynamics team and a technical university. The role requires strong skills in aerodynamics, CFD, Python programming, and an interest in aeroacoustics, supporting efficient propeller designs across various flight conditions.

Location and work setup

Location
Ottobrunn
Remote status
Hybrid
German requirement signal
No German Required Detected
Detected job language
English

Responsibilities

Conduct literature review on propeller optimization and multi-fidelity approaches; familiarize with existing design optimization frameworks; integrate aeroacoustics prediction methods; develop strategies to combine low- and high-fidelity models into a multi-fidelity optimization workflow; update and unify geometry generation, CFD simulation, and post-processing; parametrize and optimize propeller designs; validate predictions against CFD reference solutions; undertake optimization studies for flight conditions; optionally use surrogate models to enhance optimization convergence; document methodology and findings in thesis report.

Qualifications

Enrollment in a Master's program in mechanical engineering, aerospace engineering, physics, or a related field at a technical university; familiarity with CAD and CFD software, ideally Siemens NX and Ansys Fluent; foundational knowledge of aircraft and propulsion aerodynamics; basic knowledge of numerical methods and optimization; strong Python programming skills; ability to work independently and collaboratively; good written and verbal English communication skills; interest in aeroacoustics and propeller noise prediction; prior exposure to Blade Element Momentum Theory, aeroacoustics prediction methods, HPC-based simulation workflows, and surrogate models is advantageous.

Skills

Master's degree student Mechanical engineering Aerospace engineering Physics CAD software CFD software Siemens NX Ansys Fluent Aircraft aerodynamics Propulsion aerodynamics Numerical methods Optimization techniques Python programming Teamwork English communication Aeroacoustics Blade Element Momentum Theory PSU-WOPWOP HPC simulation workflows Surrogate models