Carleton University · AERO 4607

Rotorcraft Aerodynamics and Performance

Credits : 0.5 creditReference year : 2026-27

Description

Rotorcraft history and fundamentals. Momentum theory: hover, axial climb and descent, autorotation, forward flight, momentum theory for coaxial and tandem rotors. Blade element analysis. Rotor airfoil aerodynamics. Rotor blade dynamics and trim. Helicopter performance, height-velocity curves, conceptual design. High-speed rotorcraft.

Prerequisites

  • Prerequisite(s): MAAE 3004 , ( MAAE 3300 or MECH 3310 ) and MATH 3705 .

Conditions and arrangements

  • Prerequisite(s): MAAE 3004 , ( MAAE 3300 or MECH 3310 ) and MATH 3705 .
  • Lectures three hours per week.
Reference text in its original language

Rotorcraft history and fundamentals. Momentum theory: hover, axial climb and descent, autorotation, forward flight, momentum theory for coaxial and tandem rotors. Blade element analysis. Rotor airfoil aerodynamics. Rotor blade dynamics and trim. Helicopter performance, height-velocity curves, conceptual design. High-speed rotorcraft.

  • Prerequisite(s): MAAE 3004 , ( MAAE 3300 or MECH 3310 ) and MATH 3705 .
  • Lectures three hours per week.

Sources and references

Dates and sources are retained to help you verify the information. Translations are provided to facilitate reading; the official source governs conditions and requirements.

Source reference : https://calendar.carleton.ca/undergrad/courses/AERO/

Write to StudyCanada

Your plans or a question: let’s continue the conversation by email.

We will use these details to reply to your enquiry. Privacy

This form contacts StudyCanada. To contact this institution, use the details on its profile.