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Dr. Hays
Приєднався 8 чер 2018
University of Oklahoma DBF 2021 Competition Video
Video created by the 2021 OU DBF team edited by Adam Henning.
Переглядів: 186
Відео
University of Oklahoma VTOL Capstone2021
Переглядів 2183 роки тому
University of Oklahoma VTOL Capstone2021
Dr. Thomas Hays - Computational Tools in Aerospace Engineering Capstone
Переглядів 5273 роки тому
Dr. Thomas Hays - Computational Tools in Aerospace Engineering Capstone
OU BRT Argonia Cup Video 2021
Переглядів 4313 роки тому
OU Boomer Rocket Team's 2021 Argonia Cup Video created by Callen Koiner.
AME 2223 Airplane Project Fall 2020
Переглядів 1743 роки тому
Rubber Powered Airplane project results from intro to aerospace engineering during the 2020 socially distanced project. 3 second flight was the threshold goal, 8 seconds was the goal, 20 seconds rewarded bonus points.
3D Printing Tutorial
Переглядів 873 роки тому
A brief primer for how to take a CAD model, save it as an STL, slice it using repetier host, and ultimately send the Gcode to your 3d printer to start the print.
OU AIAA DBF 2020
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Final video produced by Kristine Browning and the 2019-2020 DBF team.
Thomas Nilles and Mitchell Tompkins Flight Mechanics Video
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University of Oklahoma, 2020 AME 3333 Flight Mechanics winning video from Thomas Nilles and Mitchell Tompkins. The design project RFP was for a next generation global bomber.
University of Oklahoma Boomer Rocket Team Argonia Cup 2020
Переглядів 6784 роки тому
A short video created by Cash Balke detailing the design, fabrication, and testing efforts of the OU Boomer Rocket Team for the 2020 Argonia cup competition.
Xfoil tutorial
Переглядів 44 тис.5 років тому
introduction to using Xfoil to analyze subsonic airfoil shapes.
CAM Gcode creation
Переглядів 4685 років тому
how to take a solidworks mold part and use HSM works to create Gcode to cut that file.
Mold Creation
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Overview of the difficulties posed by non-planar mold parting lines, and how to consider design for manufacturing when lofting airplanes. Examples of complex and simple mold creation are shown.
Internal Structure
Переглядів 3,5 тис.5 років тому
how to cut and layout internal structure in solidworks.
OU AME2223 Glider Competition Endurance Winner 2018
Переглядів 1305 років тому
The winning endurance glider flight from the Fall 2018 AME2223 glider competition.
Adding a Wing and Tail to the Fuselage
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Adding a Wing and Tail to the Fuselage
Solidworks 2019 Airfoil blocks and simple wings
Переглядів 3,2 тис.5 років тому
Solidworks 2019 Airfoil blocks and simple wings
University of Oklahoma CTI N5800 Rocket Launch
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University of Oklahoma CTI N5800 Rocket Launch
OU Rocket Launch November 10th Argonia Kansas
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OU Rocket Launch November 10th Argonia Kansas
University of Oklahoma Argonia Airfest Launches
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University of Oklahoma Argonia Airfest Launches
University of Oklahoma - Spednik Launch
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University of Oklahoma - Spednik Launch
University of Oklahoma - Godspeed Launch
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University of Oklahoma - Godspeed Launch
You don't change your screen on part C we can't see what you're doing
Any idea on how to fix a warning that says 'poor input coordination distribution'. Apparently, there is an excessive panel angle 40.1 at i = 26. It suggests fixing this with repaneling with PANE? What does this mean and is this something I should be concerned about? Ran the airfoil a bit in viscous mode and it seems to run fine from 0 to 18 degree AOA.
thank you. what a beautiful tutorial for a beautiful program.
Great method!
La matrice 2×2 peut être considérée comme matrice tridiagonale ?
😑 take your damn time bro
I love uuuu man so much
Nice job you Sir,
GOAT
I can't get the notepad data on a separate notepad. it only appears in the programs.. anyone who knows how to activate this with this program?
I've been struggling with the blending problem for 2 semesters, thank you for the video!
Worst experience ever
Thank you!
How to connect the xfoil with notepad for automation can you please tell me?
I am thinking GUPPY! 😱😁🤪🤣👍👍🇺🇸
But, these vehicles don't look like Blue Origin or SpaceX, ... that's VTVL! 😱😁🤪🤣👍👍🇺🇸
Quadcopter, ... Bicopter will do ya! 😱😁🤪🤣👍👍🇺🇸
😁👍👍🇺🇸
OWWW! Did not see that coming! 😱🤣👍👍🇺🇸 We can build back bigger and better! 🤣👍👍🇺🇸
I might have to go back to ssssscool! 😁👍👍🇺🇸
WHAT! These are student rockets, they have to learn to build their own motors! 😱😁🤪🤣👍👍🇺🇸
Now that's a "SOONER SCHOONER"! 😁👍👍🇺🇸
Was it actively stabilized or thinking it was a fish?! 😱😁🤪🤣👍👍🇺🇸
WOAH! We be WOBBLY! 😱😁🤪🤣👍👍🇺🇸
Sooooo, ... it makes moe betta wocket! 😱😁🤪🤣👍👍🇺🇸
Thank you for this video Doctor Hays. I have designed a small UAV for surveillance applications and was wondering which approach to use in structural skeleton design. Very much appreciated 🙏🏽
Hello, a total long shot but throwing it out there. I'm trying to duplicate an old fiberglass fuselage (40" long). I only have plans showing a side profile view and top view but need to identify a series of cross-section profiles (lofting?) to use in carving a mold plug. I've been trying many searches to see if there is software that can help creating the 3rd view cross-sections from the 2 existing views. I don't understand it, but came across your videos of Solidworks and was encouraged that maybe what I need is possible. I'm not explaining this well, but if you receive this comment and understand my question, I'd be very grateful to know if I'm looking for something that can't be done? Thank you! JGiles
you're video just made me look good at work. thank you!
how to include the L/D ratio in the pacc file as it doesnt include this parameter
I encountered an issue called "convergence failed" for viscous calculations. Airfoil is RAF 25. How can I resolve that?
I have been strugling with designing a nice wing-fuselage blend and damn it can be frustrating. I have been using the same method and tried different ones too.
This is so good dude -- make another one of these showing a full analysis of a wing, or showing advanced techniques!
You can't, it's 2D aerofoil theory
Tera bau jhyakni k padera Dr bhais a motey saaadey
Good evening Dr. Hayes, I was just asking, can you help me and create a solid works video on structural analysis of an aircraft structure
Respected Dr. Hays; my Xfoil software is not displaying Cd values. Can you suggest me a solution.
awesome! very helpful !
At 14:45 you mention there's some GUI's that go over Xfoil making it easier to make polars, etc. Would you mind sharing some insight into those? Curious what they are and how they function. Thanks and awesome tutorial otherwise.
I would recommend the Xflr5 program. Its latest version is quite stable, and you can conduct multithreaded Xfoil analysis with nice plotting. I was using it just today in fact!
Nice, would the results be more accurate if done with say ansys fluent or openfoam over solidworks cfd add on ?
Better use CATIA
Haha, I like your merciful words at the end! Any thoughts on Prandtl's non-elliptical lift distribution theory?
Thank you.
Book looks nice
Thank you for the video, it's very helpful! But I have one question, I'm pretty new at this stuff so if it's a stupid question, I'm sorry in advance :) When I follow your instructions, just three columns with values show up in the end, is there any setting on how to add a column for drag coefficient C_D which doesn't show up? Thank you!
I think you are trying to output useful polar data. look up the command "pacc" which is for polar accumulation. Xfoil has a nice user guide. Maybe also try Xflr5 which is a GUI interface for xfoil (and much more). It makes accumulating polars and viewing plots effortless. it's also free!
Hi friend, how to de-rotate airfoil please ? green line is not aligned with TR et LD edge for me. I have tried the command dero, but it doesn't work, do you have an idea how to use it, please?
you could go in and directly edit the point file, but it's likely easier to go grab a properly conditioned point file from somewhere else to start
What if I would like to obtain airfoil coordinates from the drawing??
Excellent tutorial. Cheers.
Got it!
Very interesting. I don't know why more of these have been built. A very interesting design. Thank you Dr. Hays for sharing this with the club meeting. 73 de kb5hxt
Hi Dr. Hays, I am trying to run Xfoil on my laptop using a linux sub system and am getting this error to do with fonts: Error of failed request: BadName (named color or font does not exist) Major opcode of failed request: 45 (X_OpenFont) Serial number of failed request: 26 Current serial number in output stream: 28 I don't suppose you know the solution to this? Thanks, Freya
Nice. Way to harness that huge N motor. 100+ pounds going supersonic. Awesome. Now try it with a minimum diameter rocket!