Department of Mechanical and Aerospace Engineering
(Faculty of Engineering and Design)
Aerospace Engineering (AERO) Courses
AERO 2001 [0.5 credit]
Aerospace Engineering Graphical Design
Engineering drawing techniques; fits and tolerances; working drawings; fasteners. Elementary descriptive geometry; true length, true view, and intersection of geometric entities; developments. Aerospace-specific CAD (Computer-Aided Design) assignments including production of detail and assembly drawings from actual aerospace physical models.
Aerospace Engineering Graphical Design
Engineering drawing techniques; fits and tolerances; working drawings; fasteners. Elementary descriptive geometry; true length, true view, and intersection of geometric entities; developments. Aerospace-specific CAD (Computer-Aided Design) assignments including production of detail and assembly drawings from actual aerospace physical models.
Includes: Experiential Learning Activity
Also listed as MAAE 2001.
Lectures and tutorials two hours a week, laboratory four hours a week.
Also listed as MAAE 2001.
Lectures and tutorials two hours a week, laboratory four hours a week.
AERO 3002 [0.5 credit]
Aerospace Design and Practice
Design approach and phases. Design integration. Influence of mission and other requirements on vehicle configuration. Trade-off studies, sizing and configuration layout. Flight vehicle loads, velocity-load factor diagram. Structural design: overall philosophy, role in design process, methods. Basic orbital mechanics; launch vehicle sizing.
Aerospace Design and Practice
Design approach and phases. Design integration. Influence of mission and other requirements on vehicle configuration. Trade-off studies, sizing and configuration layout. Flight vehicle loads, velocity-load factor diagram. Structural design: overall philosophy, role in design process, methods. Basic orbital mechanics; launch vehicle sizing.
Includes: Experiential Learning Activity
Prerequisite(s): AERO 2001.
Lectures three hours a week, problem analysis three hours a week.
Prerequisite(s): AERO 2001.
Lectures three hours a week, problem analysis three hours a week.
AERO 3101 [0.5 credit]
Lightweight Structures
Structural concepts; theory of elasticity; bending, torsion and shear in thin-walled beams having single or multi-cell sections; work and energy principles; deformation and force analysis of advanced structures, including stiffened thin-wall panels; finite element methods. Stability and buckling of thin-walled structures.
Lightweight Structures
Structural concepts; theory of elasticity; bending, torsion and shear in thin-walled beams having single or multi-cell sections; work and energy principles; deformation and force analysis of advanced structures, including stiffened thin-wall panels; finite element methods. Stability and buckling of thin-walled structures.
Includes: Experiential Learning Activity
Prerequisite(s): MAAE 3202.
Lectures three hours a week; problem analysis one hour a week.
Prerequisite(s): MAAE 3202.
Lectures three hours a week; problem analysis one hour a week.
AERO 3240 [0.5 credit]
Orbital Mechanics
Review of translational kinematics and dynamics. Keplerian two-body problem: Kepler's laws, orbital elements, orbit determination. Orbital perturbations: oblateness of the Earth, atmospheric drag. Orbital maneuvers and interplanetary flights. Advanced topics.
Orbital Mechanics
Review of translational kinematics and dynamics. Keplerian two-body problem: Kepler's laws, orbital elements, orbit determination. Orbital perturbations: oblateness of the Earth, atmospheric drag. Orbital maneuvers and interplanetary flights. Advanced topics.
AERO 3303 [0.5 credit]
High-Speed Flight Aerodynamics
Fundamentals of high-speed flight aerodynamics, including compressible flow, transonic and supersonic phenomena, shock waves, aerodynamic heating, and the design implications for aircraft and propulsion systems. Applications span transport aircraft, fighter jets, and high-altitude/hypersonic vehicles.
High-Speed Flight Aerodynamics
Fundamentals of high-speed flight aerodynamics, including compressible flow, transonic and supersonic phenomena, shock waves, aerodynamic heating, and the design implications for aircraft and propulsion systems. Applications span transport aircraft, fighter jets, and high-altitude/hypersonic vehicles.
Prerequisite(s): MAAE 3300 or MECH 3310.
Lectures three hours a week. Problem analysis two hours a week.
Lectures three hours a week. Problem analysis two hours a week.
AERO 3504 [0.5 credit]
Avionics I
Cockpit environment and the technologies supporting modern flight decks, evolution of the flight deck, cockpit layout, flight instruments, flight displays, situational awareness, aircraft hardware integration and testing, aircraft data networks, avionics systems architectures, air traffic control and management.
Avionics I
Cockpit environment and the technologies supporting modern flight decks, evolution of the flight deck, cockpit layout, flight instruments, flight displays, situational awareness, aircraft hardware integration and testing, aircraft data networks, avionics systems architectures, air traffic control and management.
Includes: Experiential Learning Activity
Prerequisite(s): AERO 2001 and (ELEC 2501 or ELEC 3605).
Lectures three hours a week, problem analysis and labs three hours a week.
Prerequisite(s): AERO 2001 and (ELEC 2501 or ELEC 3605).
Lectures three hours a week, problem analysis and labs three hours a week.
AERO 3700 [0.5 credit]
Aerospace Materials
Properties, behaviour and manufacturing methods for metals, polymers and ceramics used in aerospace applications. Specialty alloys for gas turbines. Properties and manufacture of aerospace composites. Behaviour of materials in space.
Aerospace Materials
Properties, behaviour and manufacturing methods for metals, polymers and ceramics used in aerospace applications. Specialty alloys for gas turbines. Properties and manufacture of aerospace composites. Behaviour of materials in space.
Includes: Experiential Learning Activity
Prerequisite(s): MAAE 2700.
Lectures three hours a week; problem analysis one hour a week.
Prerequisite(s): MAAE 2700.
Lectures three hours a week; problem analysis one hour a week.
AERO 3841 [0.5 credit]
Spacecraft Design I
Design of spacecraft and spacecraft subsystems with emphasis on mission requirements and current design methods: spacecraft configuration, payload, structural, attitude control, thermal, power, and other related subsystems. Spacecraft integration and testing.
Spacecraft Design I
Design of spacecraft and spacecraft subsystems with emphasis on mission requirements and current design methods: spacecraft configuration, payload, structural, attitude control, thermal, power, and other related subsystems. Spacecraft integration and testing.
Includes: Experiential Learning Activity
Prerequisite(s): AERO 3240 and ECOR 1032.
Lectures three hours a week, tutorials or laboratories three hours per week.
Prerequisite(s): AERO 3240 and ECOR 1032.
Lectures three hours a week, tutorials or laboratories three hours per week.
AERO 4003 [0.5 credit]
Aerospace Systems Design
Stress and deflection analysis; fatigue, safe life, damage tolerant design. Propulsion systems integration; landing gear; control and other subsystems. Mechanical component design. Airworthiness regulations and certification procedures. Weight and cost estimation and control. System reliability. Design studies of aircraft or spacecraft components.
Aerospace Systems Design
Stress and deflection analysis; fatigue, safe life, damage tolerant design. Propulsion systems integration; landing gear; control and other subsystems. Mechanical component design. Airworthiness regulations and certification procedures. Weight and cost estimation and control. System reliability. Design studies of aircraft or spacecraft components.
Includes: Experiential Learning Activity
Prerequisite(s): AERO 3002 and MATH 3705.
Lectures three hours a week, problem analysis three hours a week.
Prerequisite(s): AERO 3002 and MATH 3705.
Lectures three hours a week, problem analysis three hours a week.
AERO 4009 [0.5 credit]
Aviation Management and Certification
Product development, quality control. Strategic organizational analysis and design. Airworthiness, type certification and planning, delegation of authority, airplane flight manual. Aerospace system design and safety.
Aviation Management and Certification
Product development, quality control. Strategic organizational analysis and design. Airworthiness, type certification and planning, delegation of authority, airplane flight manual. Aerospace system design and safety.
AERO 4300 [0.5 credit]
Acoustics and Noise Control
Behaviour of compressible fluids, sound waves and properties of sound sources; measurement of sound; human perception of sound; prediction methods based on energy considerations; sound propagation in realistic environments: outdoors, rooms, ducts; absorption and transmission loss, noise control; case studies.
Acoustics and Noise Control
Behaviour of compressible fluids, sound waves and properties of sound sources; measurement of sound; human perception of sound; prediction methods based on energy considerations; sound propagation in realistic environments: outdoors, rooms, ducts; absorption and transmission loss, noise control; case studies.
Includes: Experiential Learning Activity
Prerequisite(s): MAAE 3004 and (MAAE 3300 or MECH 3310) and MATH 3705.
Lectures three hours a week.
Prerequisite(s): MAAE 3004 and (MAAE 3300 or MECH 3310) and MATH 3705.
Lectures three hours a week.
AERO 4302 [0.5 credit]
Aircraft Aerodynamics
Study of viscous and inviscid flow regions, potential flow theory, and compressibility effects. Topics include shear layers, laminar and turbulent flow, energy equations, propellor theory, and aerodynamic performance. Emphasis on lift and drag prediction, stall, separation, and high-lift device analysis.
Aircraft Aerodynamics
Study of viscous and inviscid flow regions, potential flow theory, and compressibility effects. Topics include shear layers, laminar and turbulent flow, energy equations, propellor theory, and aerodynamic performance. Emphasis on lift and drag prediction, stall, separation, and high-lift device analysis.
Includes: Experiential Learning Activity
Prerequisite(s): MAAE 3300.
Lectures three hours a week, problem analysis two hours a week.
Prerequisite(s): MAAE 3300.
Lectures three hours a week, problem analysis two hours a week.
AERO 4304 [0.5 credit]
Computational Fluid Dynamics
Governing equations of fluid motion (full & simplified). Discretization based on finite difference, finite volume, and finite element methods. Explicit and implicit integration schemes. Numerical stability. Numerical solutions of the Navier-Stokes equations: RANS, LES and DNS. Turbulence modeling. Programming-based assignments (convection/diffusion).
Computational Fluid Dynamics
Governing equations of fluid motion (full & simplified). Discretization based on finite difference, finite volume, and finite element methods. Explicit and implicit integration schemes. Numerical stability. Numerical solutions of the Navier-Stokes equations: RANS, LES and DNS. Turbulence modeling. Programming-based assignments (convection/diffusion).
Prerequisite(s): (MAAE 3300 or MECH 3310) and MATH 3705. AERO 4302 recommended.
Lectures three hours a week.
Lectures three hours a week.
AERO 4306 [0.5 credit]
Aerospace Vehicle Performance
Morphology of aircraft and spacecraft. Performance analysis of fixed wing aircraft: drag estimation, propulsion, take-off, climb and landing, endurance, payload/range, manoeuvres; operational economics. Performance analysis of rotor craft: rotor-blade motion, hovering and vertical ascent, forward flight, and autorotation. Rocket propulsion; escape velocity; orbital dynamics.
Aerospace Vehicle Performance
Morphology of aircraft and spacecraft. Performance analysis of fixed wing aircraft: drag estimation, propulsion, take-off, climb and landing, endurance, payload/range, manoeuvres; operational economics. Performance analysis of rotor craft: rotor-blade motion, hovering and vertical ascent, forward flight, and autorotation. Rocket propulsion; escape velocity; orbital dynamics.
AERO 4308 [0.5 credit]
Aircraft Stability and Control
Static stability and control: equilibrium requirements; longitudinal stability requirements; neutral points; manoeuvring flight; control forces and control requirements; lateral static stability certification requirements. Dynamic stability: axis systems; governing equations; phugoid and short period modes; lateral dynamic modes. Closed-loop control.
Aircraft Stability and Control
Static stability and control: equilibrium requirements; longitudinal stability requirements; neutral points; manoeuvring flight; control forces and control requirements; lateral static stability certification requirements. Dynamic stability: axis systems; governing equations; phugoid and short period modes; lateral dynamic modes. Closed-loop control.
AERO 4402 [0.5 credit]
Aircraft Propulsion
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.
Aircraft Propulsion
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.
AERO 4442 [0.5 credit]
Transatmospheric and Spacecraft Propulsion
Planetary/interplanetary environments and effects. Launch and spacecraft propulsion: liquid/solid/hybrid rockets, ram/scramjets, combined cycle engines, electrothermal, electromagnetic, electrostatic, nuclear, and propellantless propulsion. Trajectory analysis, multi-staging, separation dynamics. Advanced engine concepts.
Transatmospheric and Spacecraft Propulsion
Planetary/interplanetary environments and effects. Launch and spacecraft propulsion: liquid/solid/hybrid rockets, ram/scramjets, combined cycle engines, electrothermal, electromagnetic, electrostatic, nuclear, and propellantless propulsion. Trajectory analysis, multi-staging, separation dynamics. Advanced engine concepts.
AERO 4446 [0.5 credit]
Heat Transfer for Aerospace Applications
Fundamentals of heat transfer with emphasis on aerospace systems design. Conduction, convection and radiation modes of heat transfer. Radiation exchange between surfaces and view factors. Radiation in spacecraft thermal control. High speed flight and reentry heating.
Heat Transfer for Aerospace Applications
Fundamentals of heat transfer with emphasis on aerospace systems design. Conduction, convection and radiation modes of heat transfer. Radiation exchange between surfaces and view factors. Radiation in spacecraft thermal control. High speed flight and reentry heating.
Precludes additional credit for MECH 4406.
Prerequisite(s): MAAE 2400 and (MAAE 3300 or MECH 3310) and MATH 3705.
Lectures three hours a week.
Prerequisite(s): MAAE 2400 and (MAAE 3300 or MECH 3310) and MATH 3705.
Lectures three hours a week.
AERO 4504 [0.5 credit]
Avionics II
Inertial and satellite navigation systems, inertial sensor technology, design of inertial navigation systems, overview of GNSS and GPS positioning, aircraft control systems, fly-by-wire flight control, autopilot systems, EM waves and radio propagation, radio navigation aids, principles of radar, avionics communication systems and protocols.
Avionics II
Inertial and satellite navigation systems, inertial sensor technology, design of inertial navigation systems, overview of GNSS and GPS positioning, aircraft control systems, fly-by-wire flight control, autopilot systems, EM waves and radio propagation, radio navigation aids, principles of radar, avionics communication systems and protocols.
Includes: Experiential Learning Activity
Precludes additional credit for ELEC 4504 (no longer offered).
Prerequisite(s): AERO 3504 and MATH 3705. Not open to students in Electrical Engineering, Computer Systems Engineering, Engineering Physics or Communications Engineering.
Lectures three hours a week.
Precludes additional credit for ELEC 4504 (no longer offered).
Prerequisite(s): AERO 3504 and MATH 3705. Not open to students in Electrical Engineering, Computer Systems Engineering, Engineering Physics or Communications Engineering.
Lectures three hours a week.
AERO 4540 [0.5 credit]
Spacecraft Attitude Dynamics and Control
Rigid body dynamics. The dynamic behavior of spacecraft. Environmental torques. The design of attitude control systems. Gravity gradient, spin, and dual spin stabilization. Attitude manoeuvres. The design of automatic control systems. Impacts of attitude stabilization techniques on mission performance.
Spacecraft Attitude Dynamics and Control
Rigid body dynamics. The dynamic behavior of spacecraft. Environmental torques. The design of attitude control systems. Gravity gradient, spin, and dual spin stabilization. Attitude manoeuvres. The design of automatic control systems. Impacts of attitude stabilization techniques on mission performance.
AERO 4602 [0.5 credit]
Introductory Aeroelasticity
Review of structural behaviour of lifting surface elements; structural dynamics, Laplace Transforms, dynamic stability; modal analysis; flutter, Theodorsen's theory; flutter of a typical section; wing flutter, T-tail flutter, propeller whirl flutter; gust response; buffeting, limit cycle flutter.
Introductory Aeroelasticity
Review of structural behaviour of lifting surface elements; structural dynamics, Laplace Transforms, dynamic stability; modal analysis; flutter, Theodorsen's theory; flutter of a typical section; wing flutter, T-tail flutter, propeller whirl flutter; gust response; buffeting, limit cycle flutter.
AERO 4607 [0.5 credit]
Rotorcraft Aerodynamics and Performance
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.
Rotorcraft Aerodynamics and Performance
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.
AERO 4608 [0.5 credit]
Composite Materials
Reinforcing mechanisms in composite materials; material properties. Strength and elastic constants of unidirectional composites; failure criteria. Analysis of laminated plates; bending and eigenvalue problems. Environmental effects and durability. Damage tolerance. Design of composite structures.
Composite Materials
Reinforcing mechanisms in composite materials; material properties. Strength and elastic constants of unidirectional composites; failure criteria. Analysis of laminated plates; bending and eigenvalue problems. Environmental effects and durability. Damage tolerance. Design of composite structures.
AERO 4609 [0.5 credit]
Joining of Materials
Design for joining: base material and component geometry. Selection of joining method and filler material; Adhesive bonding; Soldering; Brazing; Diffusion bonding; Resistance welding; Fusion welding (GTAW, EB, laser and plasma arc); Friction welding; NDE. Emphasis on Aerospace materials and applications.
Joining of Materials
Design for joining: base material and component geometry. Selection of joining method and filler material; Adhesive bonding; Soldering; Brazing; Diffusion bonding; Resistance welding; Fusion welding (GTAW, EB, laser and plasma arc); Friction welding; NDE. Emphasis on Aerospace materials and applications.
AERO 4842 [0.5 credit]
Spacecraft Design II
System view of spacecraft. Requirements definition. Spacecraft payloads (remote sensing, imaging systems, astronomy instrumentation etc.). Exploration missions. Implications for systems and missions. Space system design case studies.
Spacecraft Design II
System view of spacecraft. Requirements definition. Spacecraft payloads (remote sensing, imaging systems, astronomy instrumentation etc.). Exploration missions. Implications for systems and missions. Space system design case studies.
Precludes additional credit for AERO 4802 (no longer offered).
Prerequisite(s): AERO 3841 and MATH 3705.
Lectures three hours a week.
Prerequisite(s): AERO 3841 and MATH 3705.
Lectures three hours a week.
Note: Not all courses listed are offered in a given year. For an up-to-date statement of course offerings for the current session and to determine the term of offering, consult the class schedule at central.carleton.ca.
Summer session: some of the courses listed in this Calendar are offered during the summer. Hours and scheduling for summer session courses will differ significantly from those reported in the fall/winter Calendar. To determine the scheduling and hours for summer session classes, consult the class schedule at central.carleton.ca