Master'sAerospace, UAM, Drones & Space Applications open

Master’s in Aerospace Acoustics and Noise Reduction Engineering

Online master's programme of 1,900 hours in aerospace acoustics and noise reduction engineering, with 12 modules covering physical acoustics and psychoacoustics, aeroacoustic theory, engine and airframe noise, computational aeroacoustics, acoustic testing and treatments, cabin noise, noise certification, airport noise and rotor and UAM noise, with an assigned technical tutor.

Duration1900 h
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute diploma
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Learning outcomes

What you will be able to do

01

Understand the fundamentals of acoustics and aircraft noise metrics.

02

Apply aeroacoustic theory to engine and airframe sources.

03

Simulate noise generation and propagation with computational methods.

04

Design acoustic treatments for nacelles and cabins.

05

Carry out acoustic tests with microphone arrays.

06

Prepare noise certification in accordance with Annex 16.

07

Assess the noise impact of airports and new UAM platforms.

Profile

Who it's for

  • Aeroacoustics engineers.
  • Noise certification engineers.
  • Airport noise specialists.
  • Acoustic test engineers.
  • Cabin vibration and comfort engineers.
  • Aviation environmental consultants.
  • Engineering or science graduates seeking to enter aircraft manufacturing.
Standards & tools

What you'll work with

  • ICAO Annex 16, Volume I (international aircraft noise standards)
  • CS-36 (EASA aircraft noise certification)
  • 14 CFR Part 36 (FAA noise standards)
  • Directive 2002/49/EC (EU environmental noise directive)
  • Regulation (EU) 598/2014 (noise-related operating restrictions at EU airports)
  • ECAC Doc 29 (noise contour calculation around civil airports)
  • ISO 3744 (sound power determination by sound pressure)
  • SAE ARP866 (atmospheric absorption of sound)
  • ANSYS Fluent
  • Simcenter 3D Acoustics
  • PowerFLOW
  • ANOPP
  • MATLAB
Syllabus

12 modules · 1900 h

  1. 1.1Wave equation and propagation
  2. 1.2Sound pressure level and the decibel
  3. 1.3One-third-octave band spectra
  4. 1.4A-weighting and PNL
  5. 1.5Effective perceived noise level (EPNL)
  6. 1.6Annoyance and exposure metrics
  7. 1.7Source directivity
  8. 1.8Atmospheric sound absorption according to ARP866
  9. 1.9Ground effects and refraction
  10. 1.10Lab: calculation of EPNL from a spectrum
  1. 2.1Lighthill's analogy
  2. 2.2Ffowcs Williams–Hawkings equation
  3. 2.3Monopole, dipole and quadrupole sources
  4. 2.4Turbulent boundary layer noise
  5. 2.5Trailing-edge noise
  6. 2.6Rotor-stator interaction noise
  7. 2.7Linearised Euler equations
  8. 2.8Propagation in non-uniform flow
  9. 2.9Kirchhoff integral methods
  10. 2.10Practical: trailing-edge noise estimation with the BPM model
  1. 3.1Fan noise: tones and broadband
  2. 3.2Jet and mixing noise
  3. 3.3Combustor noise
  4. 3.4Turbine noise
  5. 3.5Acoustic liners in nacelles
  6. 3.6Effect of bypass ratio
  7. 3.7Chevrons and serrated nozzles
  8. 3.8Open rotor and its acoustic challenge
  9. 3.9Turboprop engine noise
  10. 3.10Case study: spectrum of a turbofan on approach
  1. 4.1Landing gear noise
  2. 4.2Flap and slat noise
  3. 4.3Cavities and gaps
  4. 4.4Clean wing noise
  5. 4.5Gear fairings and noise-reduction devices
  6. 4.6Jet-flap interaction
  7. 4.7Airframe noise on approach
  8. 4.8Wind tunnel testing of airframe noise
  9. 4.9Optimisation of landing configurations
  10. 4.10Lab: CFD noise analysis of a slat
  1. 5.1LES and DES for acoustic sources
  2. 5.2Lattice-Boltzmann methods for noise sources
  3. 5.3High-order, low-dispersion schemes
  4. 5.4Non-reflecting boundary conditions
  5. 5.5Coupling between CFD and the FW-H formulation
  6. 5.6Acoustic BEM methods
  7. 5.7Rapid prediction with ANOPP
  8. 5.8Validation against tests
  9. 5.9Computational cost and hybrid strategies
  10. 5.10Lab: FW-H propagation of a cylinder in flow
  1. 6.1Anechoic chambers and acoustic wind tunnels
  2. 6.2Microphone arrays and beamforming
  3. 6.3In-flight noise measurement
  4. 6.4Instrumentation and calibration
  5. 6.5Source separation
  6. 6.6Acoustic holography techniques
  7. 6.7Liner testing in an impedance tube
  8. 6.8Certification measurement procedures
  9. 6.9Measurement uncertainty
  10. 6.10Practical: beamforming with a 64-microphone array
  1. 7.1Helmholtz resonator liners
  2. 7.2Double-layer and multi-layer liners
  3. 7.3Acoustic impedance and its modelling
  4. 7.4Porous and fibrous materials
  5. 7.5Low-frequency acoustic metamaterials
  6. 7.6Frequency-based liner optimisation
  7. 7.7Zero-splice liners
  8. 7.8Durability and maintenance
  9. 7.9Integration into composite nacelles
  10. 7.10Workshop: liner design for the BPF tone
  1. 8.1Structure-borne and airborne transmission
  2. 8.2Boundary layer noise on the fuselage
  3. 8.3Insulation with acoustic blankets
  4. 8.4Active noise control
  5. 8.5Dynamic vibration absorbers
  6. 8.6SEA for cabins
  7. 8.7ECS system noise
  8. 8.8Passenger acoustic comfort
  9. 8.9Noise in helicopter cabins
  10. 8.10Case study: acoustic treatment of a turboprop cabin
  1. 9.1ICAO Annex 16 Volume I
  2. 9.2Chapters 3, 4 and 14
  3. 9.3Measurement points: flyover, approach and lateral
  4. 9.4Data correction procedures
  5. 9.5Helicopter certification under Chapter 8
  6. 9.6Drone and eVTOL noise
  7. 9.7Equivalencies and minor changes
  8. 9.8Compliance documentation
  9. 9.9CS-36 and Part 36
  10. 9.10Case study: cumulative certification margin of a jet aircraft
  1. 10.1Noise footprint modelling
  2. 10.2ICAO balanced approach
  3. 10.3Noise abatement approach procedures
  4. 10.4Continuous descent approaches
  5. 10.5Night-time operating restrictions
  6. 10.6Strategic noise maps
  7. 10.7ECAC Doc 29 models
  8. 10.8Management of community complaints
  9. 10.9Compensation and residential sound insulation
  10. 10.10Practical: Lden contour map of an airport
  1. 11.1Blade noise: thickness and loading
  2. 11.2Blade-vortex interaction (BVI)
  3. 11.3Rotor noise in eVTOL
  4. 11.4Distributed propulsion and acoustics
  5. 11.5Drone noise in urban environments
  6. 11.6Perception of UAM noise
  7. 11.7Low-noise propellers
  8. 11.8Sonic boom noise
  9. 11.9Emerging regulations for UAM
  10. 11.10Case study: acoustic footprint of an eVTOL at take-off
  1. 12.1Selection of source and scenario
  2. 12.2Characterisation of noise sources
  3. 12.3Aeroacoustic modelling of the selected source
  4. 12.4Design of reduction measures
  5. 12.5Assessment of acoustic benefits
  6. 12.6Weight-performance trade-off analysis
  7. 12.7Validation test plan
  8. 12.8Impact on certification and operations
  9. 12.9Master's Thesis: report
  10. 12.10Master's Thesis: defence before a panel
Methodology, software & labs

How you'll learn

The programme is delivered 100% online on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. There are no fixed timetables: you progress at your own pace within the intake, so it can be combined with work.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is ANSYS Fluent, Simcenter 3D Acoustics, PowerFLOW, ANOPP and MATLAB, in free, academic or evaluation versions. Testing is studied through real procedures for microphone-array measurements in wind tunnels, liner tests in impedance tubes and airport noise mapping. Assessment is continuous by module, plus the final Master's Thesis.

Standards covered: ICAO Annex 16 to the Chicago Convention, Volume I, CS-36 (EASA), 14 CFR Part 36 (FAA), Directive 2002/49/EC, Regulation (EU) 598/2014, ECAC Doc 29, ISO 3744, SAE ARP866.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of ICAO Annex 16 Volume I, CS-36 and 14 CFR Part 36 applied to real cases, not as a theoretical annex.
Industry software:ANSYS Fluent, Simcenter 3D Acoustics, PowerFLOW, ANOPP and MATLAB, in free, academic or evaluation versions.
Master's Thesis with defence:a noise reduction project for a selected aircraft noise source, defended before a panel.
Flexible format:100% online, no fixed timetables, compatible with full-time work.
Capstone project

Build it end to end

Your final project follows the real engineering workflow, step by step, reviewed by your tutor.

Source and scenario selection
Select the noise source and scenario and characterise the sources involved.
Aeroacoustic modelling
Model the selected source with computational aeroacoustic methods.
Noise reduction measures
Design reduction measures and assess their acoustic benefits and weight trade-offs.
Validation and certification impact
Define the validation test plan and the impact on certification and operations.
Master's Thesis
Complete noise reduction project, defended before a panel.
Career opportunities

Where this takes you

Aeroacoustics engineerNoise certification engineerAirport noise specialistAcoustic test engineerCabin vibration and comfort engineerAviation environmental consultant
Admissions & scholarships

Requirements

  • A university degree in engineering, science or architecture, or equivalent demonstrable professional experience.
  • An internet connection and a computer capable of running the programme software.
  • English sufficient to read technical standards.

Ready to start?

Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.

FAQ

Frequently asked questions

The programme totals 1,900 hours over 12–14 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with ANSYS Fluent, Simcenter 3D Acoustics, PowerFLOW, ANOPP and MATLAB, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.

A SEIUM Institute diploma, awarded on passing the continuous assessment and the Master's Thesis. It is SEIUM's own qualification, not an official state degree; its recognition depends on the programme completed and the regulations of each country.

Yes. Modules passed in a course or postgraduate diploma in the same area are recognised in the higher programme. Ask about the recognition policy when you enrol.

A university degree in engineering, science or architecture (or equivalent professional experience), a computer able to run the programme software, and English sufficient to read technical standards.

Start dates are set by SEIUM's faculty for each intake. Our admissions team will confirm the next available date when you apply.

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