Turbine Blades: Creep Resistant Materials and Design

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  • เผยแพร่เมื่อ 27 พ.ย. 2024

ความคิดเห็น • 10

  • @muslimaly4053
    @muslimaly4053 3 ปีที่แล้ว +2

    Excellent lecture I have ever seen! Hats off Sir ! Lots of love and respect from Pakistan

  • @marktruong2803
    @marktruong2803 2 ปีที่แล้ว

    Great lecture! Appreciate and have an excellent health professor :)

  • @jisa98
    @jisa98 5 ปีที่แล้ว

    Nice class Professor, interesting topic.

  • @A.Lifecraft
    @A.Lifecraft 4 ปีที่แล้ว +1

    3:30 On tip clearance, i wonder if they could use a lip around the turbine front to produce a controlled separation of flow in the engine housing like they did on the SpaceShuttle main engine. With the flow separated from the housing, clearance would no longer matter that much...
    Or in other words, you create a Mach-diamond and put the turbine right in the middle of it.

    • @death_parade
      @death_parade 3 ปีที่แล้ว

      Won't the varying throttle and airflow conditions of the engine lead to change in mach diamond position and size?

    • @A.Lifecraft
      @A.Lifecraft 3 ปีที่แล้ว

      @@death_parade What i said was not to be taken literally. Yes, variations in flow would move the zone of maximum compression, still you would have useful tolerances, at least i guess so.

  • @ashokhosawad9027
    @ashokhosawad9027 5 ปีที่แล้ว

    Thank you sir. It was excellent.

  • @raccoon_from_heaven
    @raccoon_from_heaven 5 ปีที่แล้ว +2

    20:43 "vinod taxi"

    • @rajeshprasad101
      @rajeshprasad101 5 ปีที่แล้ว +2

      Thanks for point out. I should try to edit this out.

    • @amiy24
      @amiy24 3 ปีที่แล้ว

      @@rajeshprasad101 no sir, everything was great. We loved your lecture.