- Видео 14
- Просмотров 52 319
Team ARROW
Индия
Добавлен 22 сен 2015
Team ARROW is the official SAE Aerodesign Challenge Team working under SAE Nirma Collegiate Club. The team has the sole motto of working for the hobby and is one of the first organisation of Gujarat to participate in it.
We do have some ambitious projects undergoing like closed loop super endurance flight systems. Soon to be on air.
Please like, share and subscribe to our channel for more stuff on drones and Model Aircrafts.
We do have some ambitious projects undergoing like closed loop super endurance flight systems. Soon to be on air.
Please like, share and subscribe to our channel for more stuff on drones and Model Aircrafts.
FLIGHT READINESS REVIEW | TEAM ARROW | NIRMA UNIVERSITY | AUVSI SUAS 2022
FLIGHT READINESS REVIEW | TEAM ARROW | NIRMA UNIVERSITY | AUVSI SUAS 2022
Просмотров: 1 349
Видео
PROOF OF FLIGHT | TEAM ARROW | NIRMA UNIVERSITY | AUVSI SUAS 2022
Просмотров 3402 года назад
PROOF OF FLIGHT | TEAM ARROW | NIRMA UNIVERSITY | AUVSI SUAS 2022
Team Arrow Introductory Video
Просмотров 3033 года назад
Team Arrow is a student based aviation club at Institute Of Technology, Nirma University. We were first established in the year 2016 and since then we've been achieving heights both literally and achievement wise. Hope we as a club can inspire you to contribute in the aviation industry. Video Credits: Akash Tailor
Airfoil Stress and Deformation Analysis Part 2 | How to create a fine mesh in ANSYS
Просмотров 4353 года назад
The following video is the sequel of the video Airfoil Stress and Deformation analysis. In this video the parameters defined are same as the previous video but the mesh created in this iteration has higher element quality and relatively low skewness value. Video credits : Aditya Gupta Editing credits: Dev Patel
Airfoil Stress and Deformation Analysis Part 1 | ANSYS software | Team Arrow
Просмотров 1,1 тыс.3 года назад
In this video we have used Ansys workbench to simulate the stress and deformation exerted an S1223 airfoil of chord length 18cm and 3mm thickness. The circular hole on which fixed support is applied has a diameter of 5mm and is in contact with the leading edge. Video credits : Aditya Gupta Editing credits: Dev Patel
How To Cut Wing To Get Airfoil With Width in Solidworks | RC Planes | Team Arrow
Просмотров 1,5 тыс.3 года назад
This video demonstrates the procedure required to cut the wing into airfoils with certain width using Cut-Extrude feature in Solidworks 2020. This is done to reduce weight of the wing and hence enhance efficiency. If you like this video, do like, share and subscribe :) Video credits : Aditya Gupta Editing credits: Dev Patel
Swept Back Dihedral Wing Design | Easy Method | Solidworks 2020
Просмотров 8 тыс.3 года назад
Above video shows the making of a swept back dihedral wing using Solidworks 2020. Video credits : Aditya Gupta Editing credits: Dev Patel
Swept Back Wing design using Solidworks | Easy tricks | Chord-line Method
Просмотров 35 тыс.3 года назад
This is a video tutorial about construction of a swept back wing using Solidworks 2020. The method used in this video is easier than the conventional method in which you need to manipulate the coordinates in order to get the airfoil sketch. We hope this method will help you save time while creating a wing. Video credits : Aditya Gupta Editing credits: Dev Patel Stay tuned, More to come !
Team Arrow Nirma University Commercial Video AUVSI SUAS 2019
Просмотров 7105 лет назад
Team Arrow Nirma University Commercial Video AUVSI SUAS 2019
Team Arrow Nirma University Flight Readines Review AUVSI SUAS 2019
Просмотров 2 тыс.5 лет назад
Team Arrow Nirma University Flight Readines Review AUVSI SUAS 2019
Team Arrow Nirma University Proof of Flight AUVSI SUAS 2019
Просмотров 3085 лет назад
Team Arrow Nirma University Proof of Flight AUVSI SUAS 2019
Birth of a new being.
Просмотров 4017 лет назад
This video depicts the fabrication process of our new RC model aircraft.
Flight Video at SAE Aerodesign 2016- Best Design Award
Просмотров 3887 лет назад
On 20th of March 2016 history is created as Pegasus the first RC Aircraft from Gujarat is ready to perform its first sortie of the event with payload. Being the first team with the payload attached we achieved a payload fraction of 34.65 % with a staggering 325 grams of Payload Enjoy the journey of Team Arrow and the flight video at the end. Visit our FB page- TeamArrowITNU/?fref=ts
Can you please show how to design and full oblique wing with different angles.
Congrats
Any one have oblique wing design video
how did you calculate the width required and number of airfoils required ?
Hey, how is this the the sweptback wing, its just a tapered wing from both the edges
so helpful, ty so much <3
How can I give the max thickness to the airfoil as mm?
Best video with perfect Explaination to make airfoil shape 😊😊👍👍
Hello its very helpful video but my case is little different I want to make specific chord length root airfoil and also tip airfoil, need to scale them and yes also sweep angle needed but i cannot managed it as your method Plz let me know that how can i make my wing 3d model, I can share my dimentions if you want to make video for that. Waiting for your kind reply Thankyou!!!
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Nice
Great Work Team. Keep doing great. All the best for this year!
All the best for the competition!
Congratulations to your team work with high regards kgshah nana-nani
🔥
🥳🥳🥳
Great effort, all the best team
Excellent flight readiness review video and good UAS system developed. All the best!!!
All the best team for the competition
Great presentation great vehicle. All the best for the competition
Short and simple, well done!
Thank You
Thank You
Can you help me with this. When i m using loft it says rebuild error due to zero thickness .
but my airfoil when enter curve file it show open how do i closed without using line or circle ???
Brilliant! Quick and simple
Arrow rocks man!!
upgrade the team to a start up!
🛩🔝
✌🏻🥳
Great explanation of the mesh properties
@4:47
Badhiyaa...keep it up
After 0:52 there is no voice narration in this video
sorry for the inconvenience, That problem is now solved :)
Very Helpful
Superb bhai 💯💯
You’re doing great!
👌👌
Opp 🎉🎉
Amazing work!
very good tutorial!
You can simply add the Z-coordinate beside all x and y coordinates in the txt itself and the airfoil will be plotted from a certain distance equal to Z coordinate. For dihedral you could add coordinates with equivalent amount of dihedral height you require
Yes, what you said is correct. This is just a new method that we are applying here.
Helpful one🎉🎉🎉
Nice video🔥
Great work. A very helpful video too.
Very nice. Keep it up
Helpful video bro, keep it up👍👍
Congratulations To All
When you guys uploading more videos
Good job guys!!