@@prof.vanburen it’s absolutely interesting actually i am gonna take it next semester as i am studying aeronautical engineering so it would be so awesome if u do such these great videos for the propulsion system
For now, yes this is the conclusion. It is where a typical undergrad aero course would end. Over the summer or in the fall---after I wrap up the fluid dynamics series---I hope to add a few videos to this one. Topics include: hypersonics, ground vehicle aerodynamics, sports aerodynamics, and rotating systems (wind turbines, lift-based thrust, etc.)
16:48 Even when the flow is non-isentropic, like in the case of normal and oblique shocks we considered the stagnation temperature to be the same (while deriving the Prandtl relation). What is the advantage we are getting that you have mentioned here
Thanks a lot, Prof. Van Burren! Really nice playlist. It helped me a lot! Is the OneNote files, or their pdfs, available online anywhere for reference?
Glad you liked it! I will upload a PDF of all my notes to my website in the next few days. Could you send me an email at vanburenlabs@gmail.com so I can remember to let you know once they're ready?
Again, Thank you for the video Prof.Van Buren. I have a question regarding compression lift, is it possible to make a connection from it to the types of shock like in the section that starts at 18:27 and the shock expansion theory? Thank you so much Professor!
I think so! Shock expansion theory seems to be just a consideration of a system of shocks and the resulting flow properties due to those shocks---this leads to subsequent forces on the object. So inherently, these forces are connected to the types of shock in the system.
![Hypersonics [Aerodynamics #20]](http://i.ytimg.com/vi/bbaSjdYESkk/mqdefault.jpg)
![Hypersonics [Aerodynamics #20]](/img/tr.png)
![Normal shock waves [Aerodynamics #18]](http://i.ytimg.com/vi/GwNgymwwFAQ/mqdefault.jpg)
![Aerodynamic body forces and moments [Aerodynamics #3]](http://i.ytimg.com/vi/5LQxe4-BEcM/mqdefault.jpg)
Thank you so much for this playlist, Prof. Van Buren. It really helped me.
Glad you liked it!
Theses videos are THE BESTTTT
Aw thanks!
Thank you so much sir for these wonderful lectures...please keep on posting such kind of videos
I'm glad you like them! I will definitely
Thank you, Sir!
You're welcome!
We really need for this course 11:01 (propulsion systems) 🙌
Propulsion systems was one of my favorite undergrad courses!
@@prof.vanburen it’s absolutely interesting actually i am gonna take it next semester as i am studying aeronautical engineering so it would be so awesome if u do such these great videos for the propulsion system
Thank you very much for your lectures. I was making notes for my end semester test from here.
Can you please confirm if this playlist ends here???
For now, yes this is the conclusion. It is where a typical undergrad aero course would end. Over the summer or in the fall---after I wrap up the fluid dynamics series---I hope to add a few videos to this one. Topics include: hypersonics, ground vehicle aerodynamics, sports aerodynamics, and rotating systems (wind turbines, lift-based thrust, etc.)
16:48 Even when the flow is non-isentropic, like in the case of normal and oblique shocks we considered the stagnation temperature to be the same (while deriving the Prandtl relation). What is the advantage we are getting that you have mentioned here
And the stagnation pressure? From what I am seeing, it is a quantity that assumes being brought to rest isentropically.
Thanks a lot, Prof. Van Burren! Really nice playlist. It helped me a lot! Is the OneNote files, or their pdfs, available online anywhere for reference?
Glad you liked it! I will upload a PDF of all my notes to my website in the next few days. Could you send me an email at vanburenlabs@gmail.com so I can remember to let you know once they're ready?
@@prof.vanburen Done! I have sent an email.
Again, Thank you for the video Prof.Van Buren. I have a question regarding compression lift, is it possible to make a connection from it to the types of shock like in the section that starts at 18:27 and the shock expansion theory? Thank you so much Professor!
I think so! Shock expansion theory seems to be just a consideration of a system of shocks and the resulting flow properties due to those shocks---this leads to subsequent forces on the object. So inherently, these forces are connected to the types of shock in the system.
please make a course on aero design
Haha maybe! I'm not sure I have the know-how
Superb explanation ✨
But bhut chota likhte ho 😅
Thank you!