Explained: Oblique Shock Relations Derivation

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  • เผยแพร่เมื่อ 6 ก.ย. 2024
  • In this video, we will derive the oblique shock (OS) relations. We will start from integral conservation equations, and derive expressions for the downstream Mach number, density ratio, velocity ratio, pressure ratio, and temperature ratio.
    ===== RELEVANT VIDEOS =====
    → Oblique Shock Example
    goo.gl/77hjcb
    → Normal Shock Relations Derivation
    goo.gl/Unvjey
    → Normal Shock Example
    goo.gl/RBJtgV
    ===== RELEVANT LINKS =====
    ► Surface (Double) Integrals Explanation
    www.joshtheengi...
    ► VT Calculator
    www.dept.aoe.vt...
    ► MATLAB Functions
    github.com/jte...
    ===== THUMBNAIL CREDIT =====
    By Settles1 (Own work) [CC BY-SA 4.0 (creativecommon...)], via Wikimedia Commons

ความคิดเห็น • 19

  • @user-lh5nz3jf5v
    @user-lh5nz3jf5v 6 ปีที่แล้ว +1

    Hi Josh !
    I was thinking about the Oblique Shock of the rocket nozzle yesterday (overexpanded/underexpanded).
    Then, you give me the derivation for this today, I am so lucky!!!
    Thank you XD.

    • @JoshTheEngineer
      @JoshTheEngineer  6 ปีที่แล้ว +1

      My pleasure! I made this video in preparation for my discussion on overexpanded flow that I'll be doing in the next couple of weeks hopefully.

  • @SoumilSahu
    @SoumilSahu 3 ปีที่แล้ว +1

    I never understood why the tangential component of velocity stays the same across an oblique shock.
    It almost seems obvious now, thanks!

    • @JoshTheEngineer
      @JoshTheEngineer  3 ปีที่แล้ว

      You're welcome! I'm glad this helped!

  • @guruadithya9040
    @guruadithya9040 5 ปีที่แล้ว +1

    Great video! Thanks Josh

  • @benlucke7763
    @benlucke7763 5 ปีที่แล้ว +3

    Thanks so much Josh! I have my compressible flow final next Monday and you're helping me understand the material so much better. Just a quick question: was this course a part of your undergraduate curriculum?

    • @JoshTheEngineer
      @JoshTheEngineer  5 ปีที่แล้ว

      Thanks Ben! Glad I could help. Yes, we had an undergraduate compressible flow class.

    • @benlucke7763
      @benlucke7763 5 ปีที่แล้ว +1

      @@JoshTheEngineer Thanks for everything! Will spread the word about your channel to my friends.

    • @JoshTheEngineer
      @JoshTheEngineer  5 ปีที่แล้ว

      No problem! Thanks for spreading the word.

  • @xtina3237
    @xtina3237 4 ปีที่แล้ว +1

    Hi! Great video!! What about Method of Characteristic for the oblique shock?

    • @JoshTheEngineer
      @JoshTheEngineer  4 ปีที่แล้ว +1

      Thanks! I'll be going through a full derivation and application of the Method of Characteristics in a future series for sure.

    • @xtina3237
      @xtina3237 4 ปีที่แล้ว

      Wow!! That would be awesome😎.

  • @pabel4283
    @pabel4283 5 ปีที่แล้ว

    hello jhos,, it would be nice if you put subtitles in english for people who do not master the language well. Excellent video

    • @JoshTheEngineer
      @JoshTheEngineer  5 ปีที่แล้ว

      That's a good suggestion, thank you! I don't have much extra time on top of making the videos so this is tough for me to do. Also, the auto-subtitles that TH-cam can do are pretty bad, and would probably make it more confusing.

  • @nellvincervantes6233
    @nellvincervantes6233 3 ปีที่แล้ว

    Where can I find the complete derivation of the equations at 16:34 sir?

    • @JoshTheEngineer
      @JoshTheEngineer  3 ปีที่แล้ว

      I'm guessing you're talking about the normal shock relations? Here's my video on those (from the video description): th-cam.com/video/pR7mWvDWEJY/w-d-xo.html

    • @nellvincervantes6233
      @nellvincervantes6233 3 ปีที่แล้ว

      Ok thanks sir. One more question. In oblique shock, prandtl relation is also a*^2 = (u1)(u2) ?