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BEng Aeronautical and Aerospace Engineering MEng
University of Leeds — Leeds, United Kingdom
BEng Aeronautical and Aerospace Engineering MEng is a undergraduate Engineering course at University of Leeds, Leeds, United Kingdom. It takes 4 years, costs £33,700 per year and starts in September.
Undergraduate · 4 years · Full-time · Engineering · £33,700 per year
Intakes: September
Turn ideas into engineered solutions and overcome some of society’s biggest challenges. Aeronautical and aerospace engineering refers to the development of aircraft and spacecraft. It involves using science, engineering and computational and analytical skills to design vehicles and structures that interact with the Earth’s atmosphere and beyond.
Modules
- Design of Unmanned Air Vehicles for Volcano Plume Tracking
- Urban Building Surveillance
- Rainforest Fire Emergency Response
- Aeroelastic analysis of wings using low-fidelity modelling
- Design and Optimisation of a Mass-Spring-Damper system for satellite battery systems
- Conceptual Design of a Forward Swept Wing Crescent Aircraft
- Aerohydrodynamic and stability analysis of a hydroplane
- CFD machine-learning based design optimisation of transonic aircraft
Frequently asked questions
How long is BEng Aeronautical and Aerospace Engineering MEng at University of Leeds?
BEng Aeronautical and Aerospace Engineering MEng takes 4 years (Full-time).
How much does BEng Aeronautical and Aerospace Engineering MEng at University of Leeds cost?
The listed tuition fee is £33,700 per year. Fees can change, so confirm the current amount before you apply.
When does BEng Aeronautical and Aerospace Engineering MEng start?
Intakes: September.
What level is BEng Aeronautical and Aerospace Engineering MEng?
It is a undergraduate course in Engineering.
What will I study on BEng Aeronautical and Aerospace Engineering MEng?
Modules include Design of Unmanned Air Vehicles for Volcano Plume Tracking, Urban Building Surveillance, Rainforest Fire Emergency Response, Aeroelastic analysis of wings using low-fidelity modelling, Design and Optimisation of a Mass-Spring-Damper system for satellite battery systems and Conceptual Design of a Forward Swept Wing Crescent Aircraft.