Aerodynamics and performance of helicopters
| Program start date | Application deadline |
| 2026-09-01 | - |
Program Overview
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Specific Program: AMC705 - Aťrodynamique et performance des hťlicoptŤres
Prťsentation
This course is part of the university's program in mechanical engineering and is offered at the master's level.
Sommaire
- Cycle: 2e cycle (master's)
- Crťdits: 3 crťdits
- Facultť ou centre: Facultť de gťnie (engineering faculty)
- Trimestres: Automne 2026 (fall 2026)
Cible(s) de formation
The course aims to teach students to:
- Describe the types of helicopters and their control methods
- Analyze the effect of rotor types on performance
- Evaluate the performance of a helicopter in stationary, moving, ascending, and descending flight
- Optimize the geometry and operating parameters of a rotating wing
- Resolve the complex motion of a helicopter rotor subject to control movements
- Calculate the compensation and balance of a helicopter in horizontal flight
- Describe the compromises required in helicopter design
Contenu
The course covers various topics, including:
- Introduction
- Rankine-Froude theory applied to a rotor
- Blade element momentum theory (BEMT)
- Rotor motion for tilting, articulated, and rigid rotors
- Blade element theory in forward flight
- Compensation and balance of the helicopter in stationary and horizontal flight
- Performance evaluation and design considerations for helicopters
Prťalable(s)
The prerequisite for this course is IMC211.
Programmes offrant cette activitť pťdagogique (cours)
This course is offered as part of the following programs:
- Baccalaurťat en gťnie mťcanique (bachelor's in mechanical engineering)
- Doctorat en gťnie mťcanique (doctoral in mechanical engineering)
- MaÓtrise en gťnie aťrospatial (master's in aerospace engineering)
- MaÓtrise en gťnie mťcanique (master's in mechanical engineering)
