wcomp

← All comparisons

bastankhah2016_deflection — four turbines

velocitydeflectionSoftware: FLORIS, FOXES · Rotor diameter 240 m · Wind speed 9.8 m/s

View the one turbine scenario for this wake model →

Model parameters and implementation notes

The windIO inputs and their software-specific mappings are listed below. Matching literature-model names do not imply identical solver, rotor-averaging, superposition, turbulence, induction, or yaw treatments.

windIO case inputs

FLORIS

  • velocity: gaussalpha = 0.58, beta = 0.077, ka = 0.3837, kb = 0.003678
  • deflection: gaussalpha = 0.58, beta = 0.077, ka = 0.3837, kb = 0.003678

Uses sum-of-squares freestream deficit superposition (sosfs), the TurbineGrid, 3 x 3 square rotor grid with power cubic-mean, thrust cubic-mean averaging, and Crespo-Hernandez wake-added turbulence. Secondary steering, yaw-added recovery, transverse velocities, and active wake mixing are disabled.

The gauss velocity and deflection models each receive their own copy of the four input coefficients.

FOXES

  • velocity: Bastankhah2016alpha = 0.58, beta = 0.077, kTI = 0.3837, kb = 0.003678, induction = Betz, k = from kTI turbine model
  • deflection: Bastankhah2016DeflectionNo separately configured parameters

Uses Betz induction, quadratic wind-speed superposition with a local (ws_quadratic) deficit reference, grid16, 4 x 4 cell centers rotor sampling, rotor-point partial wakes, and the rotor_wd wake frame. No separate wake-added turbulence model is configured.

The ka and kb inputs configure a separate kTI turbine model; the wake model receives k=None so expansion is supplied by that turbine model.

Uses FOXES' Bastankhah2016Deflection model with Betz induction. The duplicated windIO deflection parameters are not read; the velocity-block parameters govern the calculation.

Caveat: This is a coupled comparison: yaw-dependent thrust, velocity deficit, deflection, rotor averaging, and wake superposition can all contribute to differences. It does not isolate the deflection equation.

Layout & sample locations

Turbine positions (bold, rotated by yaw angle where applicable) and the cross-section sample planes (dashed) used by the plots below.

Streamwise velocity

Cross-sections

Horizontal contour

X-Y plane at hub height.

Vertical contour

X-Z plane at Y=0 (lateral centerline).

Cross-section contour

Y-Z plane at X=20D.

Effect of aligning the configuration

Streamwise RMSE for each software pair in both configurations of this case. Thedefault andaligned views differ only in the solver settings listed at the top of the page.

Software pairDefault RMSE (m/s)Aligned RMSE (m/s)
FLORIS vs FOXES1.32001.2241

Comparison metrics

Pairwise error between software for each plotted quantity. Click a column to sort.

Software pairTargetRMSE (m/s)Max abs error (m/s)Mean abs error (m/s)NRMSE

How to interpret this comparison