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Adam Rozman
Приєднався 21 лип 2015
DEP Black Team Showcase Video
www.cecs.ucf.edu/SeniorDesignShowcase/team/distributed-electric-propulsion-black-team/
University of Central Florida
Senior Design Capstone Project
Nick Loveland, Matthew Smith, Jordan Winchell, Adam Rozman, Sean Reagan, Lucas Cavalcante
Jason as pilot!
University of Central Florida
Senior Design Capstone Project
Nick Loveland, Matthew Smith, Jordan Winchell, Adam Rozman, Sean Reagan, Lucas Cavalcante
Jason as pilot!
Переглядів: 951
Відео
DEP Plane Full Flight with Aerobatics
Переглядів 2793 роки тому
University of Central Florida Senior Capstone Project Nick Loveland, Matthew Smith, Jordan Winchell, Adam Rozman, Sean Reagan, Lucas Cavalcante Jason as pilot! 3:36 Somersault and spin recovery
Test Flight Aerobatics Short
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University of Central Florida Distributed Electric Propulsion Senior Design Project Nick Loveland, Matthew Smith, Jordan Winchell, Adam Rozman, Sean Reagan, Lucas Cavalcante Jason as pilot!
Kinematics of Mechanisms Test 1 Review
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Review of Chapters 2, 3, and 4 Copy of my notes below: drive.google.com/drive/folders/16GLN6lKNWb3ofIPst-A5tnz2fhPtCH9E?usp=share_link
ANSYS Fluent- Steady and Transient Flow Around a Cylinder of Different Reynolds Number
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ANSYS Fluent- Steady and Transient Flow Around a Cylinder of Different Reynolds Number
SLI 2017 Team Termite
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Launch Day in Huntsville Alabama for NASA Student Launch 2017. Special thanks to Tsz Pan
ANSYS Fluent - Poisseuille and Couette Flow Tutorial
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Video explaining Fluent flow simulation project 1 - Dr. Ozbay Summer 2020
thanks peter parker
thank you brother
bro thanks you're really spiderman
Hey do you have the notes for this class And would I be willing to send them to me
Hi yes, there's a link in description
La traduction en français cette si vous avez cette traduction je comprend anglais
Another question, for high re numbers you just not put laminar flow you pick the k-epsilon something, also, what is the actual difference of transient vs steady, which is the one to go if geometry is complex and rey number is high. Reynolds number for your example is changing in terms of the speed, the other factors are being the same
Here we are modeling unsteady flow using RANS, so turbulence is simulated using a model (K-epsilon in this case). Unsteady flow is a fluid quality, while transient or unsteady is just how ANSYS is treating your solution. If I run this as steady instead of transient, it will eventually reach an average solution. I'm running transient here because I want to see the shedding propagate in real time. However, steady/transient depends on your application. If you just need to find average lift and drag, you can run steady, even if there is turbulent flow, until your values average out.
i have a project for my thesis, it is a very complex geometry (submarine that looks like a drone). Its reynolds number is 67000 so for sure i need to run a transient calculation. My question is, how do you set up the inflation layers,numbers,division e.t.c every part you did or you have to do to run a cfd calculation in terms of the complexity-high reynold number.
You can do a triangles surface mesh for the 3d body. You can qualify this by a constant triangles size. Play around a bit depending on the size of your object. Generally you'll want to follow airfoil rules where you clump the points more towards the leading and trailing edge. The inflation layers are to capture boundary layers. For this case the number of layers is excessive- for your case use about 20 layers and look up a y+ spacing calculator online to figure out wall spacing given your design parameters. The wall spacing to give y+ (non dimensional parameter) equal to 1 is the size of your first inflation later.
salve para o pedrinho melhorzinho de BJ
valeu primo, entendi tudo
Hi, can i know the title of book that you get this notes from?
R.L. Norton, Design of Machinery, 6th Edition, McGraw-Hill
I need solution of norten (Solution manual for machine design (Norton 3e) -Person Prentice Hall (2006))
Wow, great job!
Hello bro Please can i get google link to the notes and all the materials you used??
This is late, but I've added a link to the textbook notes I went over in this video (and for the rest of the course)
is it paper/journal based, sir? if it yes, can you share it sir?
thanks for your tutorial <3 it helps me
Dear sir. My flow is not quite parabolic, I have tried increasing the length of the tube but the result is the same.
JAS your new TOC plane?
Shulman can fly a brick if he wants. Nice
The sheer willpower, intellect, and engineering prowess to pull off this impossible feat is astounding. UCF should start a scholarship the fine young mens names who managed to pull this off!
bet
Hi do you give Ansys fluent training if you do so please May I ask you to provide your email
I don't know why but when I open mesh, geometry doesn't load. I tried updating, also importing from external source, such as SolidWorks, still doesn't work.
Never mind, I creted another standalone, and loaded the geometry using solidworks x_t file
Hi. Can you sent to me report out this tutorial, please
peace be upon you brother Mohammed Do you have educational programs about thermodynamics, heat transfer and combustion in aeroscape domainThanks in advance
Yes, thanks I need report out, please
Is the recent iris xe graphics with the 11th gen i5 16gb ram compatible and sufficient with ansys for medium 3d simulations?
Nice
Hi Adam, thank you very much for the tutorial video. I have a question about the last component RESULTS of the Workbench project. How can I develop this last component? Where I find the numerical results to show it in my project?. Thank you again for your attention. Kind regards.
thank you,could u teach this course.
Thanks Spider-Man
HAHAHHHAHHHAHA
thank you
Start of the meshing, how can I choose the hexahedral mesh in methods?
Lol your the guy who asked if that one guy was wearing pants
Eli Egbert?
please can you upload vedeo by modeling VCCR engine
Yes please!!
your presentation is good, next lesson Try to explain clear the figures
ty spider man <3
Good job.👍🏻 Lasted almost the entire time!