Warning This site is not recommended for Internet Explorer browsers. Please use another web browser to get a better experience.

PhD Propagation of shock waves generated by a non-ducted fan: acoustic footprint along the fuselage F/H

Published
Safran Aircraft Engines Fluid Mechanics Moissy-cramayel , Ile de France , France CIFRE Full-time Master Degree First experience French Fluent English Fluent
Published

Job Description

Within the CFM RISE program, Open Fan architectures are studied to meet challenging goals in fuel consumption, gas emissions, and noise levels. In this challenging and innovative frame, the perceived noise in cabin in flight is among the key drivers. Indeed, the acoustic field produced by the propeller blades directly impinges the fuselage without attenuation or modification by a duct as in a turbomachinery. Furthermore, the propeller and aircraft speeds are beyond those of a usual propeller driven regional aircraft and the propeller aerodynamic field could be associated with shock waves. The pressure field produced by the propeller that excites the fuselage needs to be investigated to be able to evaluate the role of the propeller noise in cabin in flight, and to be able to design quieter configurations.

Applications are invited for a 3-year PhD studentship to focus on the modeling of the excitation on the fuselage caused by the propeller. Namely, the PhD student will predict the propagation of the flow field produced by the propeller up to the fuselage including non-linearity effects caused by the shock amplitudes, fuselage boundary layer refraction and airframe scattering. After a bibliographic study, the PhD student will put in place a numerical modelling using a Euler solver. In particular, a specific modelling and development will be needed to introduce the proper excitation. Then, the PhD student will perform numerical investigations to identify the impact of the different physical mechanisms and parameters. He/She will finally draw rules and simplified laws to estimate the pressure field exciting the fuselage as a function of identified driving parameters. This 3-year PhD project is part of the ARENA research program. Funded by the ANR, this is a partnership between the Ecole Centrale de Lyon (ECL) and Safran Aircraft Engines.

Job Requirements

The candidate shall possess a strong background in physical acoustics, aerodynamics, and numerical simulations.
Knowledge in turbomachinery will also be appreciated.
We are looking for highly motivated applicants with excellent interpersonal, written and oral communication skills.

Specificity of the job

The applicant will be based in LMFA (Ecully, France). Few days/weeks missions in Safran Aircraft Engines will be planned throughout the PhD. The project will involve collaboration with engineers from Safran Aircraft Engines as well as participation in national and international scientific conferences.
The working language at all locations is French although English speakers can be considered with a good understanding of the French language

Locate your future workplace

Rond Point René Ravaud - Réau 77550

Moissy-cramayel

Ile de France France

Copy Address
76,800
employees worldwide
27
Number of countries where Safran is located
35
business area families
  • © Safran