
Explore airfoil geometry and key terms, including chord line, camber line, edges, thickness ratio, camber ratio, chord length, and angle of attack, and see how shapes drive lift.
Explore how drag splits into form, skin friction, induced, and wave components, and learn design levers: streamline, high aspect ratio wings, winglets, and the use of supercritical airfoils.
Define the boundary layer as a thin surface-attached air layer mediating all aerodynamic forces. Compare laminar and turbulent regimes, laminar's low drag but higher separation risk, turbulent's stronger wall shear.
Investigate how boundary layer separation as angle of attack increases destroys the suction peak under adverse pressure gradients, leading to stall with lift loss and drag rise.
Read the airfoil lift curve: lift coefficient versus angle of attack, to understand low-speed behavior, the maximum lift coefficient, stall, cruise, climb, landing, and how flaps shift the curve upward.
Understand Reynolds number as the key to scaling aerodynamics from insects to airliners. See how inertia and viscosity shape lift, drag, and wind tunnel testing across scales.
Explore how ground effect boosts lift and reduces induced drag when a wing flies within one wingspan of the surface, reshaping takeoff and landing dynamics.
Explore three dimensional wing design elements: sweep, dihedral, and twist, and how they affect compressibility, roll stability, stall behavior, and efficiency in transport aircraft.
Explore leading edge devices—the front half of the high lift system—slats, Kruger flaps, and slots—that delay stall and boost lift, enabling low-speed takeoffs and landings, especially with trailing edge flaps.
Discover how wingtip devices, including plain tips, blended winglets, split tip winglets, and raked wingtips, reduce induced drag and cruise fuel burn by 3–6% across modern airliners.
Explore how spoilers, speed brakes, and lift dumpers manipulate lift and drag for roll control, descent, and landing. Learn their diverse implementations across modern wings.
Design supersonic wings by using thin sharp airfoils, high sweep or delta shapes, and area ruling to smooth cross-sectional area and reduce wave-drag at Mach 1 and beyond.
Explore hypersonic considerations where aerothermal heating and real gas effects dominate, making thermal protection paramount and shaping blunt leading-edge strategies and high-temperature materials like carbon-carbon composites.
Apply blade element theory to treat a propeller as a stack of airfoil sections, summing thrust and torque with twist and angle of attack, guided by diameter, pitch, and blades.
Explore piston aero engines and constant speed propellers in small general aviation aircraft; learn the four-stroke cycle, RPM control, and independent manifold pressure for efficient cruise.
Explain the turbofan architecture, where a large front fan bypasses most air around a turbojet core and bypass ratio governs thrust, fuel burn, noise, and high vs low bypass regimes.
Examine turboprops and turboshafts sharing a turbofan-like core, driving propellers or rotors via a reduction gearbox, with turboprops around 15:1 and residual exhaust, turboshafts around 100:1 and no exhaust.
Explore fighter propulsion technologies, including afterburners, variable geometry inlets, and thrust vectoring, tuned for Mach 2 supersonic flight and post-stall maneuverability.
Explore how ailerons, elevator, and rudder control roll, pitch, and yaw across the three axes, with coordinated input and autopilots blending all three for smooth flight.
Static stability on the three axes relies on the horizontal stabilizer, CG ahead of the aerodynamic center, dihedral, and the vertical fin, generating restoring moments and typical margins.
Identify the four natural dynamic modes of fixed-wing aircraft—fugoid, short period, dutch roll, and spiral—and how yaw dampers and autopilots mitigate them.
Explain fly-by-wire architecture with force sensor inputs, three identical primary computers and two dissimilar secondary computers, cross-checking and voting to command actuators at high cycle rates.
Fixed-wing aircraft are one of the most demanding engineered systems on the planet. A commercial jet integrates aerodynamics, propulsion, structures, flight controls, avionics, hydraulics, electrical power, environmental control, and airworthiness management into a package that must hold together through millions of pressurization cycles and tens of thousands of flight hours. This course walks through the complete fixed-wing stack the way a practicing aerospace engineer actually sees it and it goes deep.
Over 30 focused lessons and roughly you'll cover every subsystem, every flight regime, and every major design trade-off a working aerospace engineer has to hold in their head. Each lesson is short and visual. Instead of dense equations on a whiteboard, you'll watch boundary layers separate, shock waves form, wings flex under load, control surfaces deflect, turbofan stages spool up, landing gear extend, radar signatures shift, and maintenance tasks map onto real hardware animated on real geometry, with the key numbers and design trade-offs called out as they happen.
What makes this course different:
• Comprehensive depth, not a survey 30 lessons across 5 modules cover everything from standard-atmosphere physics to hypersonic considerations, from piston aero-engines to thrust-vectoring afterburners, from A-checks to D-checks, and the full certification basis under Part 23/25 and CS-23/25.
• Systems-level, not slide-deck-level — every module connects the physics to the hardware and the hardware to the maintenance reality.
• Animation-first lift, drag, shock waves, engine cycles, dynamic stability modes, and fly-by-wire behavior are shown in motion, not described in a paragraph.
• Works for engineers moving sideways mechanical, controls, electrical, manufacturing, and quality engineers brought into aerospace programmed will find a shared baseline here.
• Stealth and survivability treated as a proper engineering subject — shaping, planform alignment, S-ducts, radar-absorbent materials, IR-signature management, and electronic warfare are full lessons, not sidebars.
• Maintenance and airworthiness included end-to-end A/B/C/D-check structure, non-destructive inspection methods, fatigue + damage-tolerance reasoning, and certification paths are part of the curriculum, because a design that can't be maintained or certified doesn't fly.
About the instructor:
Omar Koryakin Principal Engineer. I've spent my career in precision engineering and aerospace-adjacent work, and I teach because the next generation of engineers deserves clear, visual explanations instead of decades-old textbook scans. My courses reach tens of thousands of engineers worldwide. If it can be drawn, it can be understood.
Full lesson outline (30 lessons · 5 modules)
Module 1 Aerodynamic Foundations
L01 Introduction to Fixed-Wing Flight
L02 The Atmosphere, Density, and the Standard Day
L03 Airfoil Geometry and Terminology
L04 Pressure Fields and Lift Generation
L05 Circulation, Vorticity, and the Kutta Condition
L06 Drag Decomposition: Form, Skin-Friction, Induced, Wave
Module 2 Low-Speed Aerodynamics and Stall
L07 Boundary Layers: Laminar vs Turbulent
L08 Flow Separation and Stall Mechanics
L09 Angle of Attack and the Lift Curve
L10 Reynolds Number and Aerodynamic Scaling
L11 Ground Effect and Low-Altitude Behaviour
L12 Gusts, Turbulence, and Atmospheric Disturbances
Module 3 Wings and High-Lift Systems
L13 Wing Planform, Aspect Ratio, and Span Efficiency
L14 Sweep, Dihedral, and Wing Twist
L15 Leading-Edge Devices: Slats, Krueger Flaps, Slots
L16 Trailing-Edge Flaps: Plain, Split, Slotted, Fowler
L17 Winglets, Raked Tips, and Induced-Drag Reduction
L18 Spoilers, Speed Brakes, and Lift Dumpers
Module 4 High-Speed and Transonic Aerodynamics
L19 Compressibility and Mach Number
L20 Transonic Effects and Shock-Wave Formation
L21 Supersonic Wing Design and Area Ruling
L22 Wave-Drag Management
L23 Hypersonic Considerations
L24 Aeroelasticity: Flutter, Divergence, Control Reversal
Module 5 Propulsion
L25 Propeller Aerodynamics and Blade-Element Theory
L26 Piston Aero-Engines and Constant-Speed Propellers
L27 Turbojet Thermodynamic Cycle
L28 Turbofan Cycle: Bypass Ratios Explained
L29 Turboprop and Turboshaft Cycles
L30 Afterburners, Variable-Geometry Inlets, and Thrust Vectoring