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Computing Internal Flow in a Globe Valve

Dynamic Meshing   |   Transient   |   Turbulence (k-omega SST) and 6DOF Modeling   |   Data Analysis

Minor Project 1 - Internal Flows,
Flowthermolab
09/10/2025

Project Overview

This project presents a comprehensive CFD investigation of internal flow through a globe valve to analyze:

  • Flow behavior at different valve openings
  • Discharge coefficient (Cd)
  • Mass flow rate
  • Hydrodynamic force acting on the valve
The study evaluates the valve under multiple inlet pressure conditions to understand flow characteristics and identify possible design improvements from a CFD engineering perspective.

Problem Statement

Perform Steady state, CFD Simulations for the Globe Valve Geometry, study the flow phenomenon, compare and discuss the discharge coefficient and force in y-direction over the valve for different valve openings (1mm, 3mm, 5mm, 11mm, 21mm) and evaluate performance at different inlet pressures (4 bar, 5 bar, 8 bar).

Software Used

1.   Ansys Space-Claim ------- Geometry Cleanup and refinement
2.   Ansys Fluent Mesher ----- Mesh / Grid Generation
3.   Ansys Fluent ------------- Computation
4.   Ansys Post Processor ---- Post Processing
5.   MATLAB ------------------ Data Analysis & Scientific Plots

Methodology

1. Geometry Cleanup and refinement

  • Inlet and outlet extensions were added to avoid backflow errors.
  • Internal flow domain extracted for simulation.

image
Globe Valve Geometry and Domain

2. Mesh Details

  • Focused on mesh refinement at: Valve throat, Valve seat, and Valve lift region.
  • Mesh Details:
    • Hexcore volume mesh
    • ~900,000 elements
    • Average orthogonality: 0.95
    • Y⁺ < 5
    • First layer height: 8 × 10⁻⁶ m
    • Max cell length: 1 mm
    • Min cell length: 4 mm
  • Valve Lift Cases: 1mm, 3mm, 5mm, 11mm, 21mm

image
Meshing at different valve openings (1mm, 3mm, 5mm, 11mm, 21mm)

3. Solver Settings

ParameterSetting
Solver TypePressure-Based
TimeSteady
Turbulence Modelk-ω SST
MaterialWater (Liquid)
Inlet BCPressure Inlet (4 bar, 5 bar, 8 bar)
Outlet BCPressure Outlet (3 bar)
Solver SchemeCoupled
Momentum DiscretizationQUICK Scheme
Residuals & Reports
  • Mass flow rate,
  • Y-direction force on valve
InitializationHybrid
Iterations5000–10000

Total simulation cases: 15
(5 valve openings × 3 inlet pressures)

4. Results

Velocity and Pressure Contours

Screenshot 2025-10-06 225005 Screenshot 2025-10-06 225236
Pressure & Velocity Contours at Pressure Difference 1bar, 2bar, 5bar for different valve openings

Discharge Rate & Mass Flow Rate

imageimage
Discharge Rate (Cd) & Mass Flow Rate vs valve opening in Percentage

5. Discussion & Future Scope

In this study CFD Simulations for the Globe Valve over the valve for different valve openings (1mm, 3mm, 5mm, 11mm, 21mm) for different Pressure inlet conditions (4 bar, 5 bar, 8 bar) keeping pressure outlet at 3 bar constant (for all cases). Pressure and Velocity were studied through contours understanding the pressure changes and flow rates at different location. Plot for discharge coefficient and mass flow rate.
   It can be observed from the results main pressure drop occured at the valve throat due to diminished area at less valve lift values. The inherent flow coefficient was obtained through CFD keeping the pressure difference constant for full range (1 ~ 21mm) of opening and obtained the discharge Coefficient and mass flow rate.
   Three most common flow characteristics of a valve which are called quick (fast) opening type, linear type and equal percentage type.

  • Quick opening type produces a large increase in flow rate for initial increase in valve ope is usually used for safety or cooling system where the instant large flow is required.
  • Linear type has a linear relationship between the flow rate and the valve opening that is commonly used in liquid level conrol applications.
  • Equal percentage type provides a small increase in flow rate with the initial valve openings and a significant rise with the greater openings and is widely found in pressure control and heat transfer process.
   The pressure drop was studied from the contours, the pressure at two planes that comprised of proper representation of valve opening the flow circulation and pressure changes. As it is evident from the graph represented above quick opening flow charateristic and the graph resembles the common characteristic trend for discharge rate and mass flow rate.

   Findings Summarized:
  • The data generated concluded that there were significant changes in pressure around globe valve specially in small (1mm, 3mm) valve opening, maximum force on the valve 2143.762 N was recorded at pressure difference 5bar and with valve lift the it reduced upto 90.49 N.
  • The discharge rate coefficient reduced with more valve lift decreased while the mass flow rate increased, maximum discharge coefficient 0.6012 was recorded at pressure difference 5bar Pa with minimum mass flow rate 1.54 kg.s-1recorded at pressure difference 1bar
   Future Scope:
  • Perform study to capture cavitation effects
  • Perform Preliminary Study and investigate the optimization methods
  • Optimize the design of control valve and reduce the force exerted on valve make globe valve more efficient and reduce loud noise generated from globe valve

Recommended Repository Structure

CFD-Study-Globe-Valve/
│
├── README.md
├── Geometry image
├── Mesh images
├── Fluent_Case_Files
├── Results & Data

Author:
Ansh Vishal,
Aerospace Engineer
anshvishal215@gmail.com
LinkedIn

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Studied Discharge Rate Coefficient and Mass Flow Rate at different Pressure Difference and Valve Lift

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