Description
Propulsion requirements, effects of Mach Number, altitude, and application; basic propeller, turboshaft, turbojet, turbofan; cycle analysis and optimization for gas turbine power plant; inter-relations between thermodynamic, aerodynamic and mechanical designs; rocket propulsion; selection of aeroengines.
Prerequisites
- Prerequisite(s): MAAE 2400 , MAAE 3300 and MATH 3705 .
Conditions and arrangements
- Prerequisite(s): MAAE 2400 , MAAE 3300 and MATH 3705 .
- Lectures three hours a week.
Reference text in its original language
Propulsion requirements, effects of Mach Number, altitude, and application; basic propeller, turboshaft, turbojet, turbofan; cycle analysis and optimization for gas turbine power plant; inter-relations between thermodynamic, aerodynamic and mechanical designs; rocket propulsion; selection of aeroengines.
- Prerequisite(s): MAAE 2400 , MAAE 3300 and MATH 3705 .
- Lectures three hours a 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/