JoshTheEngineer | In a Nutshell: Afterburners @JoshTheEngineer | Uploaded March 2017 | Updated October 2024, 1 hour ago.
Let's talk about what afterburners are, when they're used, and how they work. In my first 'In a Nutshell' video, I'm testing the waters on giving simplified explanations for complicated topics. Let me know what you think.
===== RELATED VIDEOS =====
→ Detailed Afterburner Video
goo.gl/nt9KBp
===== REFERENCES =====
► "Afterburners" in The Aerothermodynamics of Aircraft Gas Turbine Engines, Zukoski
► Mechanics and Thermodynamics of Propulsion, Hill and Peterson
► Aerothermodynamics of Gas Turbine and Rocket Propulsion, Oates
► Aircraft Propulsion, Farokhi
► Aerospace Propulsion Systems, Ward
► Fundamentals of Jet Propulsion with Applications, Flack
===== THUMBNAIL PHOTO CREDIT =====
By United States Navy, Mass Communications Specialist 2nd Class Michael D. Cole [Public domain], via Wikimedia Commons
Let's talk about what afterburners are, when they're used, and how they work. In my first 'In a Nutshell' video, I'm testing the waters on giving simplified explanations for complicated topics. Let me know what you think.
===== RELATED VIDEOS =====
→ Detailed Afterburner Video
goo.gl/nt9KBp
===== REFERENCES =====
► "Afterburners" in The Aerothermodynamics of Aircraft Gas Turbine Engines, Zukoski
► Mechanics and Thermodynamics of Propulsion, Hill and Peterson
► Aerothermodynamics of Gas Turbine and Rocket Propulsion, Oates
► Aircraft Propulsion, Farokhi
► Aerospace Propulsion Systems, Ward
► Fundamentals of Jet Propulsion with Applications, Flack
===== THUMBNAIL PHOTO CREDIT =====
By United States Navy, Mass Communications Specialist 2nd Class Michael D. Cole [Public domain], via Wikimedia Commons
![Explained: Angle of Attack [Airplanes]](https://i.ytimg.com/vi/Fm2Az-PgPUU/hqdefault.jpg "Explained: Angle of Attack [Airplanes]
The angle of attack (AoA) is one of the most important parameters when studying how planes fly. By definition, it is the angle between some reference line of the plane (in our case the chord line of the wing) and the relative wind. The AoA will be vital when talking about lift curves and how wings generate lift.
Chord Line: http://www.youtube.com/watch?v=Eh5W61iswSY")
![Explained: Edit Text Box GUI [MATLAB]](https://i.ytimg.com/vi/GfsClzG-fls/hqdefault.jpg "Explained: Edit Text Box GUI [MATLAB]
Edit text boxes can be used to input numbers or strings in your GUI. This video explains how create an edit text box and retrieve both string data and double data from it.")
![Explained: Assumptions for Axisymmetric Conical Flow [Taylor-Maccoll]](https://i.ytimg.com/vi/HIDeIZO0z-8/hqdefault.jpg "Explained: Assumptions for Axisymmetric Conical Flow [Taylor-Maccoll]
Its extremely important to understand the assumptions used to derive an equation. This video goes over the assumptions we will be using for the Taylor-Maccoll conical flow problem, and the impact each assumption will have later on in the derivation.")
