โšก Check Valve Slam & Air Chamber

Calculate reverse velocity slam pressure spikes during pump trip and size pneumatic air cushion surge vessel dampening.

โšก Fortran 90 Engine Double Precision (IEEE 754) โœ“ ISO / ASME Validated
Check Valve Slam & Air Chamber Fluid Mechanics
๐Ÿ“Š Solver Telemetry โ— ACTIVE
๐Ÿ‘๏ธ Views 37
โšก Solves 31
๐Ÿ’พ Downloads 488 ๐Ÿ“ฆ Fortran Code 4.4 KB
๐Ÿ“… Released Jun 2026
โฑ๏ธ Latency < 1 ms
โšก TOOLS & REPORTS:
๐Ÿ’พ Download Fortran 90
๐Ÿ’ก Hardware & Sizing Partner: Need to size a control valve or check ASME flange bolt torque for this line?
FLOWKS IEC 60534 Sizer โ†— • API 6D Valve Catalog →

โšก Check Valve Dynamic Closure & Air Vessel Surge Dampening

Real-time visual simulation of reverse flow slam and pneumatic buffer compression

๐Ÿ“ Configuration & Presets

๐Ÿ’ง Water Station (400 mm) ๐Ÿชจ Slurry Line (250 mm) ๐Ÿข High-Rise Booster (100 mm) ๐Ÿ›ข๏ธ Reflux Pump (150 mm)
๐Ÿ“ Pipeline & Acoustic Parameters
Water in steel: 1000โ€“1200 m/s, Plastic: 300โ€“500 m/s
โšก Pump Trip Deceleration & Valve Type
Typical pump trip: 2 to 15 m/sยฒ
๐Ÿ›ก๏ธ Pressure Limits & Air Vessel Protection
Key Dynamic Formulations:
โ€ข Reverse Velocity: vR = (dv/dt) ยท tclose
โ€ข Joukowsky Slam: ฮ”Pslam = ฯ ยท a ยท vR
โ€ข Peak Pressure: Ppeak = Pstatic + ฮ”Pslam
โ€ข Air Vessel: Vair = [2 A L vโ‚€ยฒ ฯ] / [2 ยท 10โต ยท ฮ”Pallow (1 + Pstat/ฮ”Pallow)]

๐Ÿ“Š Slam & Vessel Sizing Results

Configure inputs and click Compute to view results.

๐Ÿ“˜ Calculation Methodology & Engineering Theory

Dynamic Reverse Flow & Valve Slam

When a pump trips, fluid decelerates at rate $dv/dt$. Check valves take finite time $\Delta t_c$ to seat, allowing reverse flow to develop:

vR = (dv/dt) ยท tclose,    ฮ”Pslam = ฯ ยท a ยท vR

Fast-acting nozzle non-slam check valves close before significant reverse velocity builds up.

Air Cushion Vessel Sizing

Pneumatic air chambers absorb kinetic energy of the reversing fluid column through polytropic air compression, limiting peak head to $\Delta P_{allow}$.

Key Engineering Assumptions

  • Rigid or elastic pipe acoustic wave speed calculated via Korteweg equation.
  • Uniform fluid column deceleration after pump power trip.
  • Isothermal / polytropic gas compression ($n = 1.2$) inside the air vessel.