Gable-roofed Isolated Building#

Gable-roofed Isolated Building

1. Project Description#

The current study numerically reproduces the experiment Test1 from the Phase 2 report of National Institute of Standards and Technology (NIST) Aerodynamic Database [1] with AeroSim’s CFD solver.

A low-rise building with \(B \times W \times H\) dimensions:

Building Geometry

is positioned in a wind tunnel setup with 437 pressure probes distributed over its surface:

Probes Layout

The wind directions chosen to be simulated were:

Wind Directions#

Wind direction

0 \(^\circ\)

30 \(^\circ\)

60 \(^\circ\)

90 \(^\circ\)

2. Simulation Setup#

The Synthetic Eddy Method (SEM) boundary condition is applied at the inlet of the computational domain. Solid fins are distributed across the floor to ensure the desired velocity and turbulence profiles during flow development length. A Neumann boundary condition is applied at the remaining boundaries.

The building is positioned \(100H\) from inlet, and 6 grid refinement levels (\(lvl\,0\) to \(lvl\,5\)) were adopted:

Computational Grid

A 1:2 refinement ratio is estabilished between levels, and the simulation parameters at grid \(lvl\,5\) were:

Dimensionless Parameters#

\(\boldsymbol{\Delta x/B}\) (spatial resolution)

2.05e-02

\(\boldsymbol{\Delta t/CTS}\) (temporal resolution)

1.26e-03

exports/\(\boldsymbol{CTS}\) (pressure acquisition frequency)

1.00e+01

\(\boldsymbol{T/CTS}\) (statistical sample size)

3.70e+03

\(\boldsymbol{Re_{B}=U_{H}B/\nu}\)

2.25e+04

The equivalent parameters in full scale are:

Full-scale Parameters#

\(\boldsymbol{\Delta x[m]}\)

0.12

\(\boldsymbol{\Delta t[ms]}\)

0.20

\(\boldsymbol{f[Hz]}\)

61.60

\(\boldsymbol{T[s]}\)

600.00

The computational resources required were:

Computational Resources#

Device

NVIDIA L4

NVIDIA L4

NVIDIA RTX A5500

NVIDIA L4

Wind direction

0 \(^\circ\)

30 \(^\circ\)

60 \(^\circ\)

90 \(^\circ\)

Node count (million)

86.86

87.66

98.94

86.86

Allocated memory (Gb)

11.52

11.64

13.12

11.52

Ellapsed time (h)

65.96

69.30

52.84

65.98

3. Inflow#

An empty domain simulation is performed to measure the incident velocity and turbulence profiles. A probe line is placed at the position where the building will be located. The average velocities used for calculating the pressure coefficient and convective time scale are taken from this simulation.

Wind Profiles#

Inflow Profile

Wind Spectra#

The power spectral density of the velocity components at height \(H\) are compared with experimental data available in [1].

Inflow Spectrum

4. Results: Local Statistics#

The pressure coefficient is calculated using the velocity at the building height \(H\) and the reference pressure measured from a position far above the building. The same statistical processing for the pressure coefficient \(C_{p}\) peaks at each probe position is performed for both experimental and numerical data:

  • A sample of size (\(T / CTS\)) is evaluated over moving averages of the original signals, with window size of 3s.

  • The processed data is subdivided in 10 intervals, from which the minimum and maximum values will be taken for each.

  • Those min/max values are fitted to a Gumbel distribution.

  • The shape parameters from Gubel distribution are then rescaled to 3600s.

Scatter on Points Statistics#

The deviation between numerical and experimental data is quantified using the mean absolute error (MAE) and the normalized mean absolute error (NMAE):

\[\mathrm{MAE} = \frac{1}{N_{\mathrm{probes}}}\sum_{i=1}^{N_{\mathrm{probes}}}|q^{\left(i\right)}_{\mathrm{EXP}}-q^{\left(i\right)}_{\mathrm{NUM}}|\]
\[\mathrm{NMAE} = \frac{1}{N_{\mathrm{probes}}}\sum_{i=1}^{N_{\mathrm{probes}}}\frac{|q^{\left(i\right)}_{\mathrm{EXP}}-q^{\left(i\right)}_{\mathrm{NUM}}|}{\left[q^{\left(\mathrm{max}\right)}_{\mathrm{EXP}}-q^{\left(\mathrm{min}\right)}_{\mathrm{EXP}}\right]}\times 100\]
Scatter 000
Scatter 030
Scatter 060
Scatter 090

Mean and Peak Pressures#

Mean and Peaks 000
Mean and Peaks 030
Mean and Peaks 060
Mean and Peaks 090

RMS Pressures#

RMS 000
RMS 030
RMS 060
RMS 090

Skewness and Kurtosis#

Skew and Kurt 000
Skew and Kurt 030
Skew and Kurt 060
Skew and Kurt 090

Pressure Spectrum#

Cp Spectrum 000
Cp Spectrum 030
Cp Spectrum 060
Cp Spectrum 090

Execution Notes#

Execution Notes#

Execution Date (YYYY-MM-DD)

2024-11-28

Solver Version

1.6.2

Changelog#

  • 30 Oct 2024: Added scattering plots