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Cavitation in cryogenic fluids in microgravity conditions

Reference

N/A

Contract Type

PhD offer

Working Time

Full-time

Compensation

2100€ / month

Degree

Master's degree

Experience

Between 0 and 2 years

Role

Doctoral student

Application Deadline

01/03/2026

A PhD position is open in the Space Advanced Concepts Laboratory in collaboration with IMFT (institute de mécaniques des fluides des Toulouse)

Supervisors:

  • Annafederica Urbano, professor, ISA-SUPAERO
  • Sébastien Tanguy, professor, Université Paul Sabatier, IMFT

Technological context and scientific questions

During depressurization for propellant preconditioning (and cooling) prior to engine ignition or propellant transfer (in the context of space depots), bubbles can form and grow due to cavitation. This is a problem due to vapour accumulation under microgravity conditions and the impact on wall heat transfer. More generally, cavitation, under conditions where phase change predominates, is important for many applications (including nuclear power plants) and raises many questions that are not understood at the small scale.

This justifies the development of the SCREAMH2 microgravity wall cavitation experiment (currently in phase A/B development under an ESA contract), in which ISAE-SUPAERO is participating as part of the scientific team.

There are several scientific open questions regarding pool cavitation. It is unclear how the contact line phenomena (nano-region, wall roughness, cavity shape…), the level and dynamics of depressurization, and the nature of the fluid (pure or in the presence of non-condensable gas) impact the growth of these bubbles and the associated wall heat flux.

This thesis project aims to answer these questions by developing numerical models capable of accurately simulating pool cavitation, in parallel with the development of the SCREAMH2 experiment. The results will serve, on the one hand, as support for the experiment and, on the other hand, for its extension, particularly to configurations with multiple bubbles and in the presence of non-condensable gases.

Background

The present project is a continuation of the team’s recent work on the development of a solver for the direct numerical simulation of two-phase flows with phase change. The originality of the solver, based on a semi-implicit compressible projection method, lies in its thermodynamic consistency, which allows it to describe liquid, vapor, and saturation conditions at the interface for a generic fluid.

The solver has recently been extended to phase change in the presence of a contact line (solid, vapor, liquid) and validated for the simulation of nucleate boiling and pool cavitation. It has thus enabled parametric studies and model developments for bubble cavitation in microgravity at the wall. The models will be extended and generalized in this project.

This project aims to further develop the numerical solver and to use it to answer the scientific questions raised.

  1. Numerical development of the immersed boundary method [5] to include conjugate heat transfer and contact lines. After validation on basic test cases, configurations with complex geometries will need to be addressed. Initially, the simulation of CH4 pool cavitation used for validation in [4] will be reconsidered with the complex geometry (cylindrical support and cavity for the bubble).
  2. Incondensable gas. The solver will be extended to account for the presence of multi-species vapor and incondensable gases adsorption in the liquid while ensuring thermodynamic consistency at the interface. A surface tension model dependent on local composition will be developed, and the jump conditions will be adapted to take thermo-capillary effects into account. The model will need to be validated for simulation in the presence of Marangoni currents (using existing experimental data).
  3. Pool cavitation in micro-gravity. Several objectives will be pursued. The first will be to support the SCREAM H2 project with detailed numerical simulations. The second will be to extend the study of pool cavitation to many fluids, considering non-condensable gases and various geometric configurations. In particular, the phase change models developed in [4] will be extended and used to simulate multi-bubble configurations, the interaction between bubbles and their impact on wall heat transfer in microgravity.

Impact

While this project focuses on pool cavitation in microgravity, it is important to note that the developments envisaged are also intended to simulate and study other phenomena involving phase change in compressible flows in the presence of contact lines. These include 1) sloshing in tanks and 2) hydrodynamic cavitation with the development of cavitation pockets. It is planned to study such configurations towards the end of the thesis project, depending on how the project progresses.

Work environment

The PhD will be funded by CNES and will be hosted in the Space Advanced Concepts Laboratory at ISAE Supaero in collaboration with IMFT.

International Relations Intern

Reference

N/A

Working Time

Full-time

Compensation

According to current legislation

Degree

Master's degree

Experience

Between 0 and 2 years

Role

Intern

Application Deadline

15/02/2026

Within ISAE-SUPAERO, the International Relations department has the following responsibilities:

  • Proposing and managing international relations policy;
  • Representing ISAE-SUPAERO within international networks and participating in their management;
  • Drawing up, negotiating and managing international cooperation and academic exchange agreements with ISAE-SUPAERO’s partner universities and organisations, in conjunction with the Training Department;
  • Promote and facilitate incoming and outgoing mobility for students, lecturers and researchers, in support of the Training Department and the DRRP;
  • Managing funding for the outgoing mobility of students and staff.

Among the department’s activities, the trainee will be particularly involved in the Aerospace Summer Programme. This is a summer programme that welcomes around twenty foreign students and is organised every year by the schools in the ISAE group (a network of aeronautical and space engineering schools). The programme lasts six weeks, 3 of which are spent at the Institute.

Short programmes 2026: Aerospace Summer Programme

  • Contribute to the organisation of the 2026 event (in particular Welcome Guide/Pre-Departure Webinar)
  • Help welcome and monitor students when they come to campus (3 weeks in June/July)
  • Contribute to the communication of the short programmes (brochure and video)

Participate in the development of promotional tools for the Double Diploma

(incoming and outgoing mobility) in collaboration with the Mobility Department

Additional tasks:

  • Help update information about partner universities
  • Participate in setting up new collaborations with Morocco in collaboration with the ISAE Group schools

Computer Vision and Sequential Decision Making for Plant Cultivation in Bioregenerative Life Support Systems

Reference

N/A

Working Time

Full-time

Degree

Master's degree

Experience

Between 0 and 2 years

Application Deadline

13/03/2026

Bioregenerative life support systems (BLSS) are being considered for future long-duration manned space travel, as supplies from Earth are too expensive, if not impossible. Moreover, environments suitable for agriculture will also be difficult to access on Earth, mainly due to climate change and resource depletion. Both on Earth and in space, it is therefore necessary to find solutions for growing plants, which can benefit from robotics, advanced automation and machine learning, according to the scientific literature.

This internship project in artificial intelligence applied to precision agriculture aims to contribute to the development of methods for maximising long-term production and minimising resource consumption.

It focuses on optimising:

1. the estimation of the state of plants and their environment using machine learning and computer vision algorithms to monitor their growth,

2. sequential decisions using reinforcement learning algorithms to calculate autonomous cultivation strategies that are efficient and economical in the long term.

Direct Numerical Simulation of Hydrogen Bubbles Cavitation (6 months)

Contract Type

Internship offer

Degree

Master's degree

Role

Stagiaire

The objective of the present internship will be to use the DIVA code to carry out a parametric analysis on the influence of the distance between different bubbles over the wall heat transfer.

📌 Requirements: Master 2 student or equivalent interested in pursuing with a PhD thesis. Basics in computational fluid dynamics, thermodynamics, programming.

Numerical simulation of cracking in anodic films

Contract Type

Internship offer

Working Time

Full-time

Degree

Master's degree

Experience

Between 0 and 2 years

Role

Intern

2000 series aluminium alloys are widely used in the aerospace industry because of their very good specific mechanical properties.

In addition to the mechanical stresses associated with their use, aeronautical structures are also subjected to environments that can alter their integrity. Anodising surface treatments enable a thin protective film to grow, thereby improving the corrosion resistance of these alloys.

However, cracking or crazing can occur as a result of thermal stress, considerably reducing their resistance to corrosion in harsh environments. Understanding these anodic film degradation phenomena and identifying and taking into account the influencing parameters will help to improve the thermal behaviour of anodised components.

Psychoacoustic evaluation of drone noise

Contract Type

Internship offer

Working Time

Full-time

Degree

Master's degree

Experience

Between 0 and 2 years

Role

Intern

This internship proposes to evaluate the sound perception associated with multi-copter drones to allow the development of effective noise reduction strategies and awareness actions.

Flexible Aircraft Dynamics and Control

Contract Type

Internship offer

Working Time

Full-time

Compensation

600€ / month

Degree

Master's degree

Experience

Between 0 and 2 years

Role

Intern

The flexibility of aircraft structures plays a crucial role in the design of high-altitude, highly efficient, and long-endurance vehicles. For such configurations, the traditional assumption of a fully rigid airframe is no longer valid. This structural flexibility directly impacts flight dynamics, stability, and control design.

The internship offers the opportunity to contribute to an active research area at the intersection of aerodynamics, structures, and control, with potential applications in next-generation UAVs and high-altitude, long-endurance platforms.