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used <strong>to</strong> model the pneumatic transmission line<br />

Tannehill et al. (1997), which combines the<br />

lumped model (Xue and Yusop, 2005) <strong>to</strong> simulate<br />

the air dynamics in the transmission line. The<br />

experiment set‐up is shown in Figure 1.<br />

Figure 1: Experiment Set‐Up<br />

The valve is opened until the transmission line<br />

reaches a steady state. The valve is then closed<br />

and the system is allowed <strong>to</strong> reach a different<br />

steady state. Pressure transducers are used <strong>to</strong><br />

record the pressure during this process. At the<br />

same time a mass flow meter is used <strong>to</strong> record<br />

the steady state mass flow rate. The simulation<br />

is then performed <strong>to</strong> verify the transient proc‐<br />

ess of the fluid in the transmission line after the<br />

valve is fully closed.<br />

The blocked transmission line is considered <strong>to</strong><br />

have N number of segments. Hence N numbers<br />

of pressure transducers are needed <strong>to</strong> capture<br />

the changes in air pressures along a 4m polyure‐<br />

thane pneumatic transmission line which has an<br />

internal diameter of 5.0mm and a thickness of<br />

1.5mm. The change in system temperature is not<br />

considered in this study and the temperature is<br />

assumed <strong>to</strong> be constant at an ambient tempera‐<br />

ture of 20°C. The change in transmission line di‐<br />

ameter due <strong>to</strong> high system pressure is consid‐<br />

ered during the simulation.<br />

<strong>MIMET</strong> Technical Bulletin Volume 1 (2) 2010<br />

MATHEMATICAL MODEL<br />

For a general three‐dimensional Navier‐S<strong>to</strong>kes<br />

equation, the following assumptions are made:<br />

1. The swirl of the working fluid in each cross sec‐<br />

tion along the transmission line is omitted.<br />

2. The change in fluid properties along the radial<br />

direction is omitted.<br />

3. Perfect gas is considered ‐<br />

The equations are then reduced <strong>to</strong> one‐dimensional<br />

format as follows:<br />

For continuity equation:<br />

��<br />

�<br />

�t<br />

�<br />

�x<br />

��u��0 x<br />

and for momentum equation:<br />

p � � RT<br />

w<strong>here</strong> ρ is the density, ux being the velocity<br />

along the axial direction, p is the pressure, R is<br />

the gas constant, T is the system temperature<br />

and μ is the dynamic viscosity.<br />

(1)<br />

(2)<br />

| MARINE FRONTIER @ <strong>UniKL</strong><br />

107

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