
Define aerodynamics as the science of air forces and fluid motions, the interaction of gases with aircraft, and compare theoretical, experimental methods like wind tunnels and CFD.
Explore aerodynamic and inertial flying principles, examining lift from Newton's third law, drag tradeoffs with angle of attack, and a survey of fixed-wing and rotorcraft aircraft.
Explore aerodynamic schemes that shape wings, fuselage, and stabilizers to optimize lift, drag, stability, and takeoff performance across biplane and monoplane designs, including flying wing and duck plane concepts.
Explore how body-fixed and velocity-based coordinate systems in aerodynamics determine forces and moments on aircraft, and master angle of attack and sideslip definitions.
Discover how viscosity resists deformation as internal friction, shaping boundary layers and drag. Explore dynamic and kinematic viscosity, Reynolds number, and the laminar-to-turbulent transition that drives aircraft flow.
Learn how air compressibility relates to the speed of sound under isentropic assumptions. It defines Mach number and explains how velocity, temperature, and surface curvature affect compressibility.
Examine the physical properties of transonic fluids, including pressure, density, temperature, and viscosity, and how adiabatic and isentropic ideal-gas assumptions influence shock waves and boundary layers under the standard atmosphere.
Explore advanced compressibility by linking bulk modulus to density, define the speed of sound as sqrt(bulk modulus over density), and discuss Mach number effects and subsonic Bernoulli limits.
Discover how the pressure coefficient relates static and dynamic pressure, compare incompressible and compressible flows, and connect cp to Mach number and critical cp for aerodynamics.
Explore the key design parameters of swept wings, including span, leading-edge sweep, and trailing-edge sweeps. Examine taper ratio, crank location, fuselage distance, chord, thickness, camber, and angle of attack alpha.
Balance span, sweep, weight, fuel volume, and undercarriage space in wing design. Use aeroelastic considerations and fly-by-wire control for stability and efficient lift-to-drag.
Explore airfoil performance by examining lift and drag sources, including wing induced drag and parasitic skin-friction drag, and how Mach, Reynolds, and angle of attack influence lift and drag coefficients.
The supercritical airfoil enables steady transonic flight with a large leading-edge radius, flat upper surface, and rear camber to maintain lift and soften the shock.
Learn how the near-field method estimates airfoil drag by measuring surface pressure and skin friction, with CFD enabling detailed boundary layer insights while experimental sensors can disturb flow.
Apply a boundary-layer based method to estimate 3D wing drag, incorporating trailing and tip vortices, vortex drag, and the roles of circulation and downwash.
Analyze how swept wing flow separation develops spanwise with increasing incidence and shock strength. Relate pressure coefficients and two-shock patterns to predict and control separation across civil and military wings.
Step into the world of aerospace innovation with Aerospace Engineering – Complete Aerodynamics Guide, a comprehensive learning experience designed to build your mastery of the science of flight. Whether you are taking your first steps into aerospace engineering or advancing your technical expertise, this course will equip you with both the theoretical understanding and the practical skills needed to excel.
This course bridges the gap between classroom theory and real-world application. You’ll explore how aerodynamic principles shape the design and performance of aircraft, spacecraft, and even high-speed racing vehicles. With clear explanations, structured learning modules, and hands-on design exercises, you’ll gain the confidence to analyze, model, and optimize aerodynamic systems like a professional engineer.
What You’ll Learn
Core Aerodynamics Foundations: Grasp how air behaves around bodies in motion, from basic flow dynamics to complex transonic phenomena.
Transonic and High-Speed Flight: Understand the aerodynamics of commercial jets, military aircraft, and Formula One vehicles, where precision and performance intersect.
Compressibility and Viscosity Effects: Learn how air compressibility and viscosity influence lift, drag, and stability at various flight regimes.
Airfoil Design and Software Application: Gain practical experience in designing efficient airfoils using professional-grade aerodynamics software.
Advanced Concepts: Explore key topics like pressure coefficients, boundary layers, and shock waves—and learn how to interpret aerodynamic data for informed engineering decisions.
Why This Course Stands Out
Accessible Yet Comprehensive: Designed for both beginners and professionals, the course starts with the fundamentals and gradually builds up to advanced topics.
Hands-On Learning: Apply concepts through guided examples and software-based design projects to translate theory into practice.
Career-Focused Approach: Acquire skills that enhance your technical portfolio and strengthen your resume for roles in the aerospace and automotive industries.
University-Equivalent Quality: Receive a level of instruction comparable to a university course—without the high tuition costs or academic barriers.
Who This Course Is For
Aspiring Aerospace Engineers: Students and early-career professionals looking to establish a strong foundation in aerodynamics.
Engineering Professionals: Practicing engineers aiming to deepen their understanding of aerodynamic performance and design.
Aviation & Space Enthusiasts: Individuals fascinated by flight and eager to explore the physics behind aircraft and spacecraft design.
Complete Beginners: Learners with no prior background in engineering who want an approachable, step-by-step introduction to aerodynamics.
Course Requirements
No prior engineering or physics experience required—just curiosity and a willingness to learn.
A computer with internet access for viewing lectures and using design software introduced in the course.
(Optional) Basic familiarity with mathematics or physics may enhance understanding but is not essential.
Learning Outcomes
By the end of this course, you will:
Have a solid grasp of aerodynamic theory and its real-world applications.
Be able to analyze and interpret aerodynamic performance data.
Design and evaluate airfoils using simulation tools.
Understand the aerodynamic principles governing modern aircraft, spacecraft, and high-speed vehicles.
Possess the technical vocabulary and confidence to discuss and apply aerodynamic concepts in professional settings.