Aerospace Masterclass: Transonic Aerodynamics - Druckversion +- Forum Rockoldies (https://rockoldies.net/forum) +-- Forum: Fotobearbeitung - Photoshop (https://rockoldies.net/forum/forumdisplay.php?fid=16) +--- Forum: E-Learning, Tutorials (https://rockoldies.net/forum/forumdisplay.php?fid=18) +--- Thema: Aerospace Masterclass: Transonic Aerodynamics (/showthread.php?tid=63381) |
Aerospace Masterclass: Transonic Aerodynamics - Panter - 22.11.2022 Aerospace Masterclass: Transonic Aerodynamics Last updated 12/2020 MP4 | Video: h264, 1280x720 | Audio: AAC, 44.1 KHz Language: English | Size: 5.49 GB | Duration: 8h 5m Learn Aerodynamics from Beginner to Expert and How to Design Airfoils and Wings of Commercial Aircrafts What you'll learn Aircrafts classification Basic fluid dynamics Basics of aerodynamics Air compressibility effects and supersonic speeds Viscous flows including laminar and turbulent boundary layers Mach numbers, pressure coefficients and shock waves development Supercritical airfoil design Transonic 3D wing design Lift and Drag estimation techniques Aerodynamics software Advanced aerodynamics Requirements Basic high school math. Desire to learn an exciting aerospace subject Basic computer literacy Description This transonic aerodynamics course focuses on the study of the flow of air about an aircraft, but many of the concepts explored are relevant to a wide variety of applications from regular cars to Formula 1 bolides. Students completing this aerodynamics course will gain advanced understanding of concepts and techniques used to aerodynamically analyze and design transonic aircraft.All transport aircrafts today are flying in with transonic speeds, so here you will learn everything you need to know for designing commercial aircraft such as Boeing or Airbus. The course will end by practical exercise where you will apply everything you have learned to design your own airfoil using a on open source software. What you will learn?:Aircrafts classificationBasic fluid dynamicsBasics of aerodynamicsAir compressibility effects and supersonic speedsViscous flows including laminar and turbulent boundary layersMach numbers, pressure coefficients and shock waves developmentSupercritical airfoil designTransonic 3D wing designLift and Drag estimation techniquesAerodynamics software Overview Section 1: Introduction Lecture 1 Introduction Lecture 2 Why Learning Aerodynamics? Lecture 3 What Aerodynamics Is All About? Section 2: Aircraft Types and Purpose Lecture 4 Flying Principles and Aerostatics Principle Lecture 5 Aerodynamic and Inertial Flying Principles Lecture 6 Aircraft Components and Usage Lecture 7 Aerodynamic Schemes Section 3: Basic Aerodynamics Lecture 8 Coordinate Systems Lecture 9 Forces and Moments Lecture 10 General Atmosphere Information Lecture 11 Viscosity and Viscous Flows Lecture 12 Air Compressibility Lecture 13 Branches in Aerodynamics Section 4: Transonic Flow Fundamentals Lecture 14 What is Transonic Flow? Lecture 15 Physical Properties of Transonic Fluids Lecture 16 Advanced Compressibility Lecture 17 Pressure Coefficient Lecture 18 Mach Waves and Shock Waves Section 5: Transonic Airfoil Lecture 19 2D Airfoils Lecture 20 Compressibility Effects for Airfoils Lecture 21 Shock Waves on Airfoils Lecture 22 Viscous Flows Lecture 23 Boundary Layers on Airfoils Lecture 24 Viscous Flow Effects on Airfoils Lecture 25 Shock-Induced Separation for Airfoils Section 6: Real 3D Swept Wings Lecture 26 Classification of the Aircrafts Lecture 27 Definition of Swept Wing Lecture 28 General Design Considerations Lecture 29 Application of Wing Sweep Lecture 30 Swept Wing Design: Part 1 Lecture 31 Swept Wing Design: Part 2 Lecture 32 Swept Wing Performance Lecture 33 Military Swept Wing Design Section 7: Transonic Airfoil Performance Lecture 34 Airfoil Performance Background Lecture 35 Transonic Airfoil Characteristics Lecture 36 Compressibility and Wave Drag Lecture 37 General Drag Definition and Prediction Lecture 38 The Supercritical Airfoil Lecture 39 Drag Prediction | Near - Field Method Lecture 40 Drag Prediction | Far - Field Method Lecture 41 Example of Drag Calculation Lecture 42 Example of Calculation of Shock Induced Separation Lecture 43 Types of Shock Induced Separation Section 8: Swept Wing Performance Lecture 44 Boundary Layer Performance Method Lecture 45 Lift Dependent and Skin Friction Drag Method Lecture 46 Swept Wing Flow Separation Section 9: Software Tools For Aerodynamics Lecture 47 Aerodynamics Software: XFoil Section 10: Conclusions Lecture 48 How To Use What You've Learned? Lecture 49 What Comes Next In Aerospace Engineering? Lecture 50 Bonus Lecture: Discount Coupons Mechanical Engineers,Aerospace Engineers,Avionics Engineers,Aeronautical Engineers,Aerospace Engineering Students,Employees in the aerospace sector with no engineering background,Space lovers Download from RapidGator Download from DDownload |