What you'll learn
Understand the Fundamentals of Aerodynamics
Understand the Compressible Aerodynamics
Understand the Incompressible Aerodynamics
Understand how Airplanes generate lift and drag
Understand the Concept of Mach Number
Requirements
Basic physics (High School Level) Not mandatory
Interest in Aeronautical and Aerospace Engineering
Interest in Aviation
Interest in Airplane
Description
The Fundamentals of Aircraft Aerodynamics: Aerospace and Aeronautical Engineering Fundamentals Course is a multidisciplinary course where you will study the Fundamentals of Aerodynamics, Shock Waves, Mach Number. My intention is that you fully understand the main topics regarding Aerodynamics and Aeronautical Engineering Fundamentals.The structure of the Course is the following:IntroductionFundamentals of AerodynamicsCompressible AerodynamicsIncompressible AerodynamicsShock WavesFour ForcesDifference between Compressible and Incompressible AerodynamicsControl Surfaces Mach NumberReynolds NumberBoundary layerWe will discuss topics such as Mach Numbers, Reynolds Number, Boundary layer and Control Surfaces and much more!The objective of the Course are for you to understand how Airplanes is able to fly, how compressible and incompressible aerodynamics affects airplane, how the Drag is Generated in Aircraft as well as Lift related to the Drag, difference between compressible and Incompressible aerodynamics and why? control surfaces, Mach Number and Performance of the Aircraft depending on the Range and Weights.I encourage you to begin this journey to Fundamentals of Aircraft Aerodynamics - Aerospace and Aeronautical Engineering, you won't regret it! If you have any doubts during the course feel free to ask me or contact me and clarify it immediately, I will answer as quick as possible!My aim is to convince you that Engineering and specifically Aeronautical Engineering are topics which can be faced if one is interested in them.I hope you find the courses useful and enjoy the material uploaded!Kind Regards to all!Lakshmanan Kuppanchetty N,India.
Overview
Section 1: Short Introduction
Lecture 1 Course Overview
Lecture 2 Short Introduction
Lecture 3 Components of Airplane
Lecture 4 Usage of Components
Section 2: Compressible & Incompressible Aerodynamics
Lecture 5 Compressible Aerodynamics
Lecture 6 Incompressible Aerodynamics
Section 3: Control Surfaces
Lecture 7 Control Surface
Lecture 8 Secondary Control Surfaces
Lecture 9 How the control surfaces working
Section 4: Fundamentals of Aerodynamics
Lecture 10 Fundamentals of Aerodynamics
Lecture 11 Types of Drag
Lecture 12 Lift Drag Calculations
Lecture 13 Stalling in Aircraft
Section 5: Shock waves
Lecture 14 Shock waves
Section 6: Mach Number, Reynolds Number and Boundary Layer
Lecture 15 Mach Number
Lecture 16 Reynolds Number Calculation
Lecture 17 Boundary Layer
Science Students,Aeronautical Students,Engineers


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