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CFD study of a Bézier nozzle vs Laval: smoother shocks, lower wall force, better flow stability

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Axisymmetric CFD Analysis of a Bézier-Shaped Nozzle

2D axisymmetric compressible-flow simulation of a nozzle with a Bézier-curve wall profile, compared with a conventional De Laval nozzle under the same boundary conditions.

ANSYS Fluent Model Flow

Mach

← Baseline study: De Laval nozzle analysis


Objective

The study looks at how a smooth Bézier wall contour changes three things compared with a conventional De Laval profile:

  • choked flow
  • shock structure
  • wall loading

Both nozzles use the same boundary conditions, similar mesh densities (≈ 450–500k cells) and the same number of iterations.

Simulation Setup

Parameter Value
Geometry 2D axisymmetric
Inlet / outlet diameter 10 mm / 7.5 mm
Fluid Air, ideal gas
Inlet pressure 200,000 Pa
Outlet pressure 0 Pa (gauge)
Solver Pressure-based, steady
Turbulence model SST k-ω
Energy equation On
Mesh ≈ 460,000 cells
Iterations 2000

Results

Integral quantities

Quantity Value
Inlet mass flow rate 0.0133 kg/s
Outlet mass flow rate 0.0125 kg/s
Mass imbalance ≈ 6.0 %
Wall force ≈ 270 N
Inlet mass flow Outlet mass flow Wall force
Mass_Inlet Mass_Outlet Wall Force

Flow fields

Pressure Velocity magnitude
Pressure Velocity
Temperature Density
Temperature Density
Convergence history

Scaled Residuals


Observations (Bézier vs. De Laval)

  • Shock structure: In the Bézier nozzle the shock transitions are more diffuse and less abrupt. The smooth, continuously curved wall spreads the pressure gradients out. The De Laval nozzle, with sharper geometric transitions, shows more distinct shocks and separation zones.
  • Wall loading: The Bézier nozzle gives a lower wall force (≈ 270 N vs. ≈ 583 N) because the flow accelerates and decelerates more gently.
  • Mass balance: The inlet/outlet imbalance is smaller for the Bézier nozzle (6.0 % vs. 8.7 %).

These first results suggest that the Bézier contour gives smoother flow with weaker shocks. The mass imbalances of both nozzles are still above normal convergence targets (< 0.5 %), so the comparison should be read as qualitative. The next step is a tighter convergence check with a density-based solver.


Author

Burak Yörükçü · GitHub · burakyorukcu@outlook.com

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CFD study of a Bézier nozzle vs Laval: smoother shocks, lower wall force, better flow stability

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