Uploaded June 2013 | Updated September 2026, 2 weeks ago
JoshTheEngineer
|
Explained: Pitch Stiffness [Flight Dynamics]
🔇 TAP TO UNMUTE
![Explained: Pitch Stiffness [Flight Dynamics]](https://i.ytimg.com/vi/bo68hptU6YA/mqdefault.jpg "Explained: Pitch Stiffness [Flight Dynamics]
Explained: Pitch Stiffness [Flight Dynamics]")
![Explained: Static Text GUI [MATLAB]](https://i.ytimg.com/vi/cWZLGpaVwwE/mqdefault.jpg "Explained: Static Text GUI [MATLAB]
Static text fields can be used to indicate the status of your program, or simply to write text or numbers. This video describes how to set the static text field in a MATLAB GUI.")
![Explained: Critical Mach Number [Airplanes]](https://i.ytimg.com/vi/e3BWJZIvXQ4/mqdefault.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/mqdefault.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/mqdefault.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/mqdefault.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: Pitch Stiffness [Flight Dynamics] @JoshTheEngineer](https://i.ytimg.com/vi/bo68hptU6YA/maxresdefault.jpg)
