Startseite ICEEM07: Three-Dimensional Flow Optimization of a Pneumatic Pulsator Nozzle with a Continuous Adjoint
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ICEEM07: Three-Dimensional Flow Optimization of a Pneumatic Pulsator Nozzle with a Continuous Adjoint

  • Krzysztof J. Wołosz EMAIL logo und Jacek Wernik
Veröffentlicht/Copyright: 22. Januar 2015
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Abstract

The article presents results of multi-criteria optimization of air nozzle topology. The optimization in the Computational Fluid Dynamics (CFD) has been recently developed since equations of flow in porous media were applied among others governing equations. Optimization is a seeking for extremum of an objective function with respect to the function constraints. With this definition in mind, the optimization by using a continuous adjoint for the current cases is a finding such channel topology which minimizes for example pressure or energy loss when the constraints of objective function are in the form of flow governing equations of momentum and continuity. This methodology of optimization makes a design process faster comparing to the methods related to Design of Experiments (DoE). However, for the sake of flow governing equations nonlinearity, the continuous adjoint method can be successfully applied only in relatively simply and steady-state cases. The method consists in seeking of a global extremum of objective function. This extremum can sometimes be find in only simple and stationary events. The results of optimization of two selected cases are presented in the article and show advantages and limitations of the method applied. The continuous adjoint simulation results indicate the nozzles design directions and can be applied in industry with limited reliability. The object of research reported in the article is the nozzle which is augmented equipment used with a pneumatic pulsator. The pulsators are devices that utilize an air stream to destruct vaults created in loose material structure. The pulsator productivity equipped with a nozzle depends on outlet pressure. Therefore, the optimization problem was stated so that pressure loss is to be as low as possible.

Nomenclature

Abbreviations

CFD

Computational Fluid Dynamics

CFD-O

CFD – Optimization

DoE

Design of Experiments

Symbols

Dh

Hydraulic diameter m

F

Vector of unit body forces m/s2

I

Turbulence intensity

J

Objective function

L

Lagrange function

R

Vector of residuals of governing equations solutions

Re

Reynolds number

S

Surface m2

F

Vector of unit body forces m/s2

S=nS

Surface vector m2

V

Volume m/s3

k

Turbulent kinetic energy J/kg

l

Turbulent length scale m

n

Normal vector

p

Pressure Pa

pt

Total pressure Pa

p˜

Adjoint pressure Pa

t

Time s

u

Velocity vector Pa

u˜

Adjoint velocity vector m/s

un

Magnitude of velocity normal to the boundary m/s

α

Porosity

ρ

Density kg/m3

μ

Dynamic viscosity Pas

ν

Kinematic viscosity m2/s

νT

Kinematic eddy viscosity m2/s

ω

Specific dissipation rate 1/s

Indexes

i

cell number

in

inlet boundary

out

outlet boundary

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Received: 2014-3-20
Accepted: 2014-11-14
Published Online: 2015-1-22
Published in Print: 2015-2-1

©2015 by De Gruyter

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