JoshTheEngineer | Explained: Conservation of Energy @JoshTheEngineer | Uploaded June 2016 | Updated October 2024, 1 hour ago.
In this video, we will derive the conservation of energy equation in integral form using a control volume fixed in space. We start with the simple equation for the first law of thermodynamics, and apply it to our control volume with flow passing through its control surface.
===== LINKS TO OTHER VIDEOS =====
1D Conservation of Energy
goo.gl/mmbe9a
===== OTHER REFERENCES =====
Good explanation of all the terms in the equation along with derivation:
Computational Fluid Dynamics, John Anderson
My favorite derivation of the conservation equations in index notation
Fundamental Mechanics of Fluids, I.G. Currie
If you want a great CFD book with the derivations also included
Computational Fluid Mechanics and Heat Transfer, Tannehill, Anderson, and Pletcher
In this video, we will derive the conservation of energy equation in integral form using a control volume fixed in space. We start with the simple equation for the first law of thermodynamics, and apply it to our control volume with flow passing through its control surface.
===== LINKS TO OTHER VIDEOS =====
1D Conservation of Energy
goo.gl/mmbe9a
===== OTHER REFERENCES =====
Good explanation of all the terms in the equation along with derivation:
Computational Fluid Dynamics, John Anderson
My favorite derivation of the conservation equations in index notation
Fundamental Mechanics of Fluids, I.G. Currie
If you want a great CFD book with the derivations also included
Computational Fluid Mechanics and Heat Transfer, Tannehill, Anderson, and Pletcher
![Explained: Critical Mach Number [Airplanes]](https://i.ytimg.com/vi/e3BWJZIvXQ4/hqdefault.jpg "Explained: Critical Mach Number [Airplanes]
Explained: Critical Mach Number [Airplanes]")
![Explained: NACA 4-Digit GUI Part 8/10 [MATLAB]](https://i.ytimg.com/vi/eW8eEJtwRqA/hqdefault.jpg "Explained: NACA 4-Digit GUI Part 8/10 [MATLAB]
This is the eighth video in my 10-video series on coding a program in MATLAB to compute, display, and save a NACA 4-digit airfoil.
IN THIS VIDEO:
We code the radio button for showing the camber line of the airfoil. We also code the Exit button.
Radio Button Video:
https://goo.gl/E4Owva
Exit Button Video:
https://goo.gl/aarwmW
IN THIS SERIES:
Part 1/10 : https://goo.gl/9UBgbo
Part 2/10 : https://goo.gl/jRRcYJ
Part 3/10 : https://goo.gl/rSVLHo
Part 4/10 : https://goo.gl/HwHB39
Part 5/10 : https://goo.gl/AlDne8
Part 6/10 : https://goo.gl/7n1QP7
Part 7/10 : https://goo.gl/nTGleR
Part 8/10 : https://goo.gl/ez247P
Part 9/10 : https://goo.gl/8mXYcc
Part 10/10: https://goo.gl/ovBlbW")
![Explained: Populate a Listbox [MATLAB]](https://i.ytimg.com/vi/esZVttsTQ9I/hqdefault.jpg "Explained: Populate a Listbox [MATLAB]
This video explains how to select files from a folder and make those file names visible in a listbox.")
![Explained: Continuity Equation for Axisymmetric Conical Flow [Taylor-Maccoll]](https://i.ytimg.com/vi/f79k_ZWtCdc/hqdefault.jpg "Explained: Continuity Equation for Axisymmetric Conical Flow [Taylor-Maccoll]
The continuity (conservation of mass) equation was derived in a previous video. Since the Taylor-Maccoll problem is formulated in spherical coordinates, the conservation equation needs to be recast in terms of spherical coordinates. A few of the assumptions discussed in the previous assumptions video are used to simplify the equation to a useful form for this problem.
The links to relevant videos can be found here.
Continuity Equation
http://www.youtube.com/watch?v=uXPRyYAHvZk
Taylor-Maccoll Assumptions
http://www.youtube.com/watch?v=HIDeIZO0z-8")
![Explained: Sound Suppression Water System [Space Shuttle]](https://i.ytimg.com/vi/fc1WokD1A1c/hqdefault.jpg "Explained: Sound Suppression Water System [Space Shuttle]
The acoustic waves generated from the space shuttle as it lifts off have the potential to damage both the launch structure as well as the shuttle itself. Water is used to absorb some of this energy to ensure a safe launch.
After seeing a different view in a video, it appears that the SSME exhaust hole water nozzles shoot water horizontally across the hole from the sides. The nozzles look like theyre located towards the top of the exhaust hole.
A couple videos that have excellent footage of the structure can be seen below. Note: I would turn down your volume a little before clicking the links because youve probably turned it up to watch my videos.
http://www.youtube.com/watch?v=ezVOSfbKNJ0
http://www.youtube.com/watch?v=dTAjGiZvI9k
This video is pretty spectacular too.
https://www.youtube.com/watch?v=mjrpuG2HOuI")
![Explained: Irrotational Condition [Taylor-Maccoll]](https://i.ytimg.com/vi/g4vnuSHBokU/hqdefault.jpg "Explained: Irrotational Condition [Taylor-Maccoll]
Croccos equation (under our given assumptions) led to an expression regarding the irrotationality of the flow. That is, the flow is free from rotation. Expanding the expression that the curl of the velocity field is zero, another expression relating the velocities flow can be obtained.")
