Aeronautical Engineer Course

Lesson 1 • Introduction to Fluid Mechanics

This module establishes continuity, momentum, and energy equations for fluid flow. It forms the physical basis for aerodynamics and propulsion analysis.

Lesson 2 • Thermodynamics and Heat Transfer

This module introduces thermodynamic cycles, gas laws, and heat transfer modes relevant to propulsion and thermal management. It directly supports engine and thermal analysis chapters.

Lesson 3 • Mathematics for Aerospace Applications

This module covers vector calculus, differential equations, and linear algebra essential to aerospace analysis. It provides the mathematical toolkit used throughout all subsequent chapters.

Lesson 4 • Materials Science for Aerospace

This module surveys metallic, composite, and ceramic materials used in aircraft. It connects material properties to structural design decisions made in later chapters.

Lesson 1 • Airfoil Theory and Performance

This topic analyzes pressure distribution, lift generation, and drag on 2D airfoil sections. It establishes the aerodynamic building block for wing and body analysis.

Lesson 2 • Viscous Flow and Boundary Layers

This topic analyzes laminar and turbulent boundary layer development, transition, and separation. It connects viscous effects to skin friction drag and stall prediction.

Lesson 3 • Compressible and High-Speed Flow

This topic covers isentropic flow, normal and oblique shocks, and expansion fans for high-speed regimes. It prepares students for supersonic aircraft and inlet design.

Lesson 4 • Finite Wing Aerodynamics

This topic extends 2D airfoil theory to 3D finite wings using lifting-line and vortex-lattice methods. It quantifies induced drag and span efficiency for wing design.

Lesson 1 • Equations of Motion for Aircraft

This topic derives 6-DOF equations of motion for a rigid aircraft in atmospheric flight. It provides the dynamic framework for performance and stability analysis.

Lesson 2 • Takeoff and Landing Performance

This topic analyzes ground roll, rotation, obstacle clearance, and landing distances. It connects aerodynamic and propulsion data to airfield performance requirements.

Lesson 3 • Maneuvering Flight and Agility

This topic examines turning flight, V-n diagrams, and energy maneuverability for both civil and military aircraft. It links structural load limits to operational flight envelopes.

Lesson 4 • Range, Endurance, and Mission Analysis

This topic applies Breguet equations and mission segment analysis to compute range and endurance. It enables fuel fraction estimation for conceptual design.

Lesson 1 • Inlets, Nozzles, and Diffusers

This topic analyzes subsonic and supersonic inlet design, nozzle expansion, and pressure recovery. It connects component efficiency to overall engine performance.

Lesson 2 • Compressors and Turbines

This topic covers axial and centrifugal compressor design, turbine stage analysis, and efficiency maps. It provides tools for matching components in an engine cycle.

Lesson 3 • Air-Breathing Engine Fundamentals

This topic introduces turbojet, turbofan, turboprop, and ramjet cycles using ideal and real thermodynamic analysis. It establishes performance metrics used throughout propulsion design.

Lesson 4 • Rocket Propulsion Principles

This topic analyzes chemical rocket performance, nozzle design, and propellant selection for launch and spacecraft applications. It extends propulsion knowledge beyond air-breathing systems.

Lesson 1 • Stress, Strain, and Elasticity

This topic reviews stress-strain relationships, Hooke's law, and failure criteria for aerospace materials. It provides the continuum mechanics foundation for structural analysis.

Lesson 2 • Buckling and Stability of Structures

This topic covers Euler column buckling, plate buckling, and post-buckling behavior in thin-walled structures. It is essential for sizing compression-loaded panels and stringers.

Lesson 3 • Aircraft Load Cases and V-n Diagrams

This topic defines design load cases from maneuver, gust, and ground loads per airworthiness standards. It connects flight mechanics to structural sizing requirements.

Lesson 4 • Bending, Shear, and Torsion of Beams

This topic analyzes bending moments, shear flow, and torsion in open and closed thin-walled sections. It is directly applicable to wing spars, fuselage frames, and control surfaces.

Lesson 1 • Dynamic Stability Modes

This topic analyzes phugoid, short-period, Dutch roll, spiral, and roll modes using linearized equations. It connects modal characteristics to pilot handling quality criteria.

Lesson 2 • Static Stability and Trim

This topic evaluates longitudinal, lateral, and directional static stability using aerodynamic derivatives. It establishes trim conditions and stability margin requirements.

Lesson 3 • Advanced Control and Agility

This topic covers active flutter suppression, envelope protection, and carefree handling for high-performance aircraft. It extends control design to nonlinear and limit regimes.

Lesson 4 • Control Surface Design and Sizing

This topic sizes elevators, ailerons, and rudders to meet control authority and hinge moment requirements. It links aerodynamic derivatives to control surface geometry.

Lesson 1 • System Safety and Reliability Analysis

This topic applies fault tree analysis, FMEA, and safety assessment processes to aircraft systems. It connects system design to airworthiness certification requirements.

Lesson 2 • Environmental Control and Pressurization

This topic analyzes cabin pressurization, air conditioning, and oxygen systems for crew and passenger safety. It links thermodynamic principles to life-support system design.

Lesson 3 • Hydraulic and Actuation Systems

This topic analyzes hydraulic power generation, distribution, and actuator design for flight controls and landing gear. It connects system architecture to reliability and redundancy.

Lesson 4 • Electrical Power Systems

This topic covers AC and DC power generation, distribution buses, and more-electric aircraft concepts. It supports understanding of avionics and system electrification trends.

Lesson 1 • Weight Estimation and Balance

This topic applies statistical and analytical weight estimation methods to size major structural groups. It determines CG travel and verifies balance across the loading envelope.

Lesson 2 • Aerodynamic and Propulsion Integration

This topic refines aerodynamic polars and integrates propulsion sizing with aircraft performance targets. It closes the design loop between aerodynamics, propulsion, and weight.

Lesson 3 • Design Review and Iteration

This topic conducts formal design review, identifies closure issues, and iterates the design to convergence. It develops professional design documentation and presentation skills.

Lesson 4 • Structural Concept and Systems Layout

This topic defines primary structural concept, load paths, and systems installation within the airframe. It prepares the design for detailed structural and systems analysis.

Lesson 5 • Configuration Selection and Layout

This topic evaluates fuselage, wing, empennage, and propulsion configurations using trade studies. It produces an initial three-view layout and internal arrangement.