Aeronautical Engineer Course

Lesson 1 • Introduction to Fluid Mechanics

Establishes continuity, momentum, and energy equations for fluid flow. Forms the physical basis for aerodynamics and propulsion analysis.

Lesson 2 • Thermodynamics and Heat Transfer

Introduces thermodynamic cycles, gas laws, and heat transfer modes relevant to propulsion and thermal management. Directly supports engine and thermal analysis chapters.

Lesson 3 • Mathematics for Aerospace Applications

Covers vector calculus, differential equations, and linear algebra essential to aerospace analysis. Provides the mathematical toolkit used throughout all subsequent chapters.

Lesson 4 • Materials Science for Aerospace

Surveys metallic, composite, and ceramic materials used in aircraft. Connects material properties to structural design decisions made in later chapters.

Lesson 1 • Airfoil Theory and Performance

Analyses pressure distribution, lift generation, and drag on 2D airfoil sections. Establishes the aerodynamic building block for wing and body analysis.

Lesson 2 • Viscous Flow and Boundary Layers

Analyses laminar and turbulent boundary layer development, transition, and separation. Connects viscous effects to skin friction drag and stall prediction.

Lesson 3 • Compressible and High-Speed Flow

Covers isentropic flow, normal and oblique shocks, and expansion fans for high-speed regimes. Prepares students for supersonic aircraft and inlet design.

Lesson 4 • Finite Wing Aerodynamics

Extends 2D airfoil theory to 3D finite wings using lifting-line and vortex-lattice methods. Quantifies induced drag and span efficiency for wing design.

Lesson 1 • Equations of Motion for Aircraft

Derives 6-DOF equations of motion for a rigid aircraft in atmospheric flight. Provides the dynamic framework for performance and stability analysis.

Lesson 2 • Takeoff and Landing Performance

Analyses ground roll, rotation, obstacle clearance, and landing distances. Connects aerodynamic and propulsion data to airfield performance requirements.

Lesson 3 • Manoeuvring Flight and Agility

Examines turning flight, V-n diagrams, and energy manoeuvrability for both civil and military aircraft. Links structural load limits to operational flight envelopes.

Lesson 4 • Range, Endurance, and Mission Analysis

Applies Breguet equations and mission segment analysis to compute range and endurance. Enables fuel fraction estimation for conceptual design.

Lesson 1 • Inlets, Nozzles, and Diffusers

Analyses subsonic and supersonic inlet design, nozzle expansion, and pressure recovery. Connects component efficiency to overall engine performance.

Lesson 2 • Compressors and Turbines

Covers axial and centrifugal compressor design, turbine stage analysis, and efficiency maps. Provides tools for matching components in an engine cycle.

Lesson 3 • Air-Breathing Engine Fundamentals

Introduces turbojet, turbofan, turboprop, and ramjet cycles using ideal and real thermodynamic analysis. Establishes performance metrics used throughout propulsion design.

Lesson 4 • Rocket Propulsion Principles

Analyses chemical rocket performance, nozzle design, and propellant selection for launch and spacecraft applications. Extends propulsion knowledge beyond air-breathing systems.

Lesson 1 • Stress, Strain, and Elasticity

Reviews stress-strain relationships, Hooke's law, and failure criteria for aerospace materials. Provides the continuum mechanics foundation for structural analysis.

Lesson 2 • Buckling and Stability of Structures

Covers Euler column buckling, plate buckling, and post-buckling behaviour in thin-walled structures. Essential for sizing compression-loaded panels and stringers.

Lesson 3 • Aircraft Load Cases and V-n Diagrams

Defines design load cases from manoeuvre, gust, and ground loads per airworthiness standards. Connects flight mechanics to structural sizing requirements.

Lesson 4 • Bending, Shear, and Torsion of Beams

Analyses bending moments, shear flow, and torsion in open and closed thin-walled sections. Directly applicable to wing spars, fuselage frames, and control surfaces.

Lesson 1 • Dynamic Stability Modes

Analyses phugoid, short-period, Dutch roll, spiral, and roll modes using linearised equations. Connects modal characteristics to pilot handling quality criteria.

Lesson 2 • Static Stability and Trim

Evaluates longitudinal, lateral, and directional static stability using aerodynamic derivatives. Establishes trim conditions and stability margin requirements.

Lesson 3 • Advanced Control and Agility

Covers active flutter suppression, envelope protection, and carefree handling for high-performance aircraft. Extends control design to nonlinear and limit regimes.

Lesson 4 • Control Surface Design and Sizing

Sizes elevators, ailerons, and rudders to meet control authority and hinge moment requirements. Links aerodynamic derivatives to control surface geometry.

Lesson 1 • System Safety and Reliability Analysis

Applies fault tree analysis, FMEA, and safety assessment processes to aircraft systems. Connects system design to airworthiness certification requirements.

Lesson 2 • Environmental Control and Pressurisation

Analyses cabin pressurisation, air conditioning, and oxygen systems for crew and passenger safety. Links thermodynamic principles to life-support system design.

Lesson 3 • Hydraulic and Actuation Systems

Analyses hydraulic power generation, distribution, and actuator design for flight controls and landing gear. Connects system architecture to reliability and redundancy.

Lesson 4 • Electrical Power Systems

Covers AC and DC power generation, distribution buses, and more-electric aircraft concepts. Supports understanding of avionics and system electrification trends.

Lesson 1 • Weight Estimation and Balance

Applies statistical and analytical weight estimation methods to size major structural groups. Determines CG travel and verifies balance across the loading envelope.

Lesson 2 • Aerodynamic and Propulsion Integration

Refines aerodynamic polars and integrates propulsion sizing with aircraft performance targets. Closes the design loop between aerodynamics, propulsion, and weight.

Lesson 3 • Design Review and Iteration

Conducts formal design review, identifies closure issues, and iterates the design to convergence. Develops professional design documentation and presentation skills.

Lesson 4 • Structural Concept and Systems Layout

Defines primary structural concept, load paths, and systems installation within the airframe. Prepares the design for detailed structural and systems analysis.

Lesson 5 • Configuration Selection and Layout

Evaluates fuselage, wing, empennage, and propulsion configurations using trade studies. Produces an initial three-view layout and internal arrangement.