Chevy TBI head exhaust throat experiment, Throat ratio 87.8% winner!

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  • Опубликовано: 8 сен 2024
  • Up the ratio and got some gains.

Комментарии • 30

  • @mikkokuorttinen3113
    @mikkokuorttinen3113 2 месяца назад +2

    Thank you Charles! Well done with this port! The audience is happy

  • @dondotterer24
    @dondotterer24 2 месяца назад +1

    Charlie. Thanks for doing all the hard work and time. Not boring we will all learn from it. Very interesting.

  • @robtdougherty
    @robtdougherty 2 месяца назад +3

    Short one, NOT Boring! love it! thanks, thats a great looking port

  • @nw4167
    @nw4167 2 месяца назад

    Don't forget that the exhaust heat is a natural accelerant. So it doesn't act the same way as the intake. In other words, it doesn't hurt to make your throat size a little bigger.

  • @theshed8802
    @theshed8802 2 месяца назад +2

    Not boring at all Charlie

  • @Patrick-xd8jv
    @Patrick-xd8jv 2 месяца назад +1

    Looks purdy

  • @luckyPiston
    @luckyPiston 2 месяца назад +1

    So this throat mod countered the SSR center velocity gain from the last mod , but overall flow was improved , so are we seeing a correlation here between the throat area and the profile of the SSR ?

  • @chrisstavro4698
    @chrisstavro4698 2 месяца назад +1

    I calculated 1.411" throat which is 88.2%. Just my rule of thumb. What kind of valve job will you do on that?

  • @rolandotillit2867
    @rolandotillit2867 2 месяца назад +2

    How did the average airspeed change? I bet you it changed less than half a percent. So weighing up the flow gains vs speed loss, I'd still call it a win overall.

    • @luckyPiston
      @luckyPiston 2 месяца назад +2

      Isnt it just a win at subsonic speeds were unbalanced velocities don't effect density as much ? but at higher velocities , transonic and so forth cant unbalanced velocities and densities turn into turbulence ? it may not be a win if its not relatively balanced , i/m assuming exhaust gases can go supersonic maybe im wrong in that assumption...

    • @rolandotillit2867
      @rolandotillit2867 2 месяца назад +2

      @@luckyPiston You are right they can, at very low lifts, because the pressure difference between the chamber and the port is such that you will get a sonic shock at the valve margin right when the valve comes off the seat. At that point, until around .200 lift, it is a supersonic diffuser, after that the valve/seat interface transitions to a subsonic diffuser. In that transition phase is where the most dangerous disturbance to flow occurs, as you correctly pointed out.
      *I will add, that this happens long before the piston starts it's travel from BDC.
      **On a four valve it would be closer to .100 lift.

    • @luckyPiston
      @luckyPiston 2 месяца назад +1

      @@rolandotillit2867 Very interesting

  • @tchapps88
    @tchapps88 2 месяца назад +2

    Is there enough meat on the roof to mimick a tpi/lt1 D port?

    • @servediocylinderheads
      @servediocylinderheads  2 месяца назад +1

      @@tchapps88 Roof is basically stock.

    • @tchapps88
      @tchapps88 2 месяца назад +1

      @@servediocylinderheads i was asking if the roof had enough material to be raised into a D port

    • @servediocylinderheads
      @servediocylinderheads  2 месяца назад +1

      @@tchapps88 It is stock thickness now.

    • @luckyPiston
      @luckyPiston 2 месяца назад +1

      5 videos back he did a show n tell on a sliced in 1/2 (193) ex port check it out .

  • @seanbrown8269
    @seanbrown8269 2 месяца назад +5

    The 90% rule of thumb is just that. It doesn't scale well and assumes that the throat is the minimum cross section in the port. Valve lift, chamber shape, valve size, and the placement of the minimum cross section will all play role, and then it's down to what you're doing with your Valve job.

    • @luckyPiston
      @luckyPiston 2 месяца назад +2

      The radii on the SSR seems to be a significant player too ..