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Oblique shocks and expansion fans [Aerodynamics #19] 

Prof. Van Buren
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In this video we continue our exploration of shocks by moving on to Oblique Shocks and Expansion Fans. Oblique shocks occur when the flow angles inwards which creates a shock angled to the flow. They are essentially the same as Normal Shocks, though we only worry about the normal component of velocity passing through the shock. Expansion fans are different, they have thickness to them and the changes to the flow are gradual. They occur when the flow opens, but in this case velocity increases and not decreases, as with normal/oblique shocks. We also discuss the forces on the body to the shock.
Free downloadable notes (PDF with white background) can be found at my website: sites.udel.edu/vanburen/educa...

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9 июл 2024

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Комментарии : 24   
@nicollelucena9152
@nicollelucena9152 3 года назад
Thank you so much for this playlist, Prof. Van Buren. It really helped me.
@prof.vanburen
@prof.vanburen 3 года назад
Glad you liked it!
@ED-zp3wu
@ED-zp3wu 7 месяцев назад
Theses videos are THE BESTTTT
@prof.vanburen
@prof.vanburen 6 месяцев назад
Aw thanks!
@evangelinblessyhknzrypjimp4972
@evangelinblessyhknzrypjimp4972 3 года назад
Thank you so much sir for these wonderful lectures...please keep on posting such kind of videos
@prof.vanburen
@prof.vanburen 3 года назад
I'm glad you like them! I will definitely
@engineers_hub
@engineers_hub 5 месяцев назад
Thank you, Sir!
@prof.vanburen
@prof.vanburen 2 месяца назад
You're welcome!
@kushmandey6880
@kushmandey6880 3 года назад
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???
@prof.vanburen
@prof.vanburen 3 года назад
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.)
@seridiscover-101
@seridiscover-101 11 месяцев назад
We really need for this course 11:01 (propulsion systems) 🙌
@prof.vanburen
@prof.vanburen 10 месяцев назад
Propulsion systems was one of my favorite undergrad courses!
@ahmadal-areeqy9881
@ahmadal-areeqy9881 10 месяцев назад
@@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
@wonderfulcat7362
@wonderfulcat7362 3 года назад
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?
@prof.vanburen
@prof.vanburen 3 года назад
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?
@wonderfulcat7362
@wonderfulcat7362 3 года назад
@@prof.vanburen Done! I have sent an email.
@gloxe1282
@gloxe1282 Год назад
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!
@prof.vanburen
@prof.vanburen Год назад
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.
@tom_winguill
@tom_winguill Год назад
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
@prof.vanburen
@prof.vanburen Год назад
And the stagnation pressure? From what I am seeing, it is a quantity that assumes being brought to rest isentropically.
@tom_winguill
@tom_winguill Год назад
please make a course on aero design
@prof.vanburen
@prof.vanburen Год назад
Haha maybe! I'm not sure I have the know-how
@Kamnarautela89637
@Kamnarautela89637 5 месяцев назад
Superb explanation ✨ But bhut chota likhte ho 😅
@prof.vanburen
@prof.vanburen 2 месяца назад
Thank you!
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