Design of Kaplan Turbine | Part-2: MATLAB Code & SolidWorks Design | Xdynemo

[@abuaseel2903]

You are a wonderful (Eng-artist) with a beautiful mind, that is a perfect presentation.I hope you win paradise.

[@NikhilSaiprasannaD]

Very well done nd presented 🔥👍🏻.

[@mechdesignbedo8449]

Thank you

[@adolfooyarzun]

this is so great, thank u so much for this, this is so helpful for my grade work

[@dhawalraja9035]

you are great ...... can you tell where you get training for writing a matlab code ?

[@chucknorris9511]

Best training is to use it and figure it out on your own. I learned by forcing myself to use it in certain classes when I had the option to use Excel instead. I am quite comfortable with Matlab now.

[@lombarekbenflis585]

How did you get 0.0985 the distance between the plan in solid work and the diamètres of circle in video at 19.02min ?

[@aashishchhantyal6907]

Why did u choose naca airfoil 4412 ??? Sir

[@Metalhead_070]

Where did you get the chord length relation from? What will be the chord length for NACA 2412 ?

[@queenefayethtaganas6706]

Good day! I am Queene Fayeth Taganas. A fourth year Mechanical Engineering student. Is it okay to use your matlab code for Kaplan turbine for my Thesis? Hoping for your response soon. Thank you!

[@jorgeluistorresrodriguez927]

Wow your channel is pure gold! Amazing, do you have LinkedIn? Congrats! I hope that you upload more videos.👍

[@Xdynemo]

Thanks for the comment. www.linkedin.com/company/xdynemo www.linkedin.com/in/chandanvarmamamalla

[@yaba5804]

Hi, great video. What about the steps after the runner and hub design is complete, like the part where the spindle follows the link generator. Do you have any good advice?

[@georgetusingwiremutetweka401]

I like this however, in reality the runner blade profile section thickness is bigger at the hub and goes on becoming smaller towards the tip of the blade. Is it possible to manually change the profle of the blade at each diameter to realise this

[@siriosystems3799]

Really very clear explanation! 2 question: naca profile in a section is oriented as a function of B1. But is B2 angle at trailing edge respected? And is it correct to consider Vw1 constant at different distance from center of flow?

[@krypton1886]

Почему не отсекли края лопастей под цилиндр?

[@onderekmekci8614]

beyond great .... Super ++++++ super

[@harshadajadhav2869]

please design francis Turbine

[@lombarekbenflis585]

You are amazing and your explanation is very clear and simple Can you leave the link of code MATLAB in description or send with email ?