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Applications for Advanced Masters remain open until August 18 for French and European applicants, as well as for non-European applicants who already hold a visa.

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Research Engineer – Structural Dynamics

Reference

N/A

Contract Type

Fixed-term contract

Working Time

Full-time

Degree

PhD

Application Deadline

31/12/2026

The engineer will contribute to all work packages within the CRÉSAT project, playing a central role in experimental developments. Their work will be carried out in close collaboration with a postdoctoral researcher recruited for the project at the École de l’Air et de l’Espace (EAE).

Their tasks will focus primarily on the preliminary design and development of several deployable-structure prototypes, with increasing fidelity, ranging from beam-type structures to truss-type architectures. Particular attention will be paid to replicating operational conditions, notably in microgravity environments and under shock-type loads. The dynamic characterisation of the various systems will provide input for the project’s numerical models.

The project is based on an innovative approach combining hybrid control and a wave-based representation of structural behaviour. Based on the phenomena of wave propagation, reflection and absorption, this approach notably introduces the concept of anechoic termination, which aims to limit unwanted reflections and confine vibrational energy. The hybrid control system will therefore aim to implement this type of termination experimentally. In this context, the engineer will play a key role in the experimental validation and development of the control strategy, initially passive and subsequently hybrid. In particular, he or she will be involved in the design of control laws and their real-time implementation using data acquisition systems (such as dSPACE).

Finally, particular attention will be paid to identifying and accounting for any non-linear phenomena, notably those induced by the junctions between the various structural elements.

Control of wingtip vortices via inhomogeneous jet injection

Reference

N/A

Working Time

Full-time

Compensation

3400€ / MONTH

Degree

PhD

Experience

Between 2 and 5 years

Role

Post-doctoral research assistant

Application Deadline

01/09/2026

This experimental project aims to investigate the control of wingtip vortices through the injection of variable-density jets into the vortex core, with the objective of accelerating their destabilisation and decay. This approach is motivated by the significant applied relevance of such vortices, which contribute to the formation of condensation trails in aircraft wakes and, consequently, to aviation-induced radiative forcing. The primary diagnostic technique employed is time-resolved Particle Image Velocimetry (PIV), enabling precise quantification of the vortex dynamical response to the induced perturbations. The project builds upon recent numerical findings from the research group, which demonstrated considerable transient growth potential in variable-density vortices, as well as preliminary experimental measurements already successfully carried out on the department’s test bench.

Project Acoudrone : Towards Silent Drones

Working Time

Full-time

Degree

PhD

Installed propeller acoustics via Body Force Modeling

Working Time

Full-time

Degree

PhD

Role

Post-doctoral student

NUMERICAL SIMULATIONS OF TURBOPROP AEROELASTICITY

Degree

PhD

Role

Post-doc position

ISAE-SUPAERO and Ratier-Figeac are seeking for a candidate holding a PhD degree in one or more of the related fields (propeller aerodynamics, aeroelasticity, numerical simulations).
He/she should demonstrate ability to work in team and interact with team members (from ISAE-SUPAERO, Ratier-Figeac and other members of the consortium) via regular reporting.
Knowledge in StarCCM+ and aeroacoustics is a plus.

Dynamic Soaring

Working Time

Full-time

Compensation

Based on experience

Degree

PhD

Are you passionate about aerodynamics, flight dynamics and new propulsion strategies? Join our team to explore Dynamic Soaring, a flight technique inspired by seabirds that increases the endurance of UAVs by exploiting wind gradients. This postdoctorate offers a unique opportunity to combine experimental measurements and advanced simulations to better understand and control this innovative flight strategy.

Dynamic Soaring (DS) is a flight strategy that exploits wind gradients to increase the energy of an aircraft without active propulsion. Inspired by seabirds, this technique extracts kinetic energy from wind variations, thereby improving the endurance of UAVs in flight.

This postdoctorate is part of advanced research aimed at better understanding and exploiting this strategy by combining experimental measurements and flight dynamics simulations.

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