OzzieFlow
Mechanical
- Feb 10, 2011
- 9
I'm trying to obtain a proper understanding of buoyancy-driven flow. My main question is whether the shape of the temperature profile throughout the length of the pipe has any influence on the pressure difference created?
Consider a vertical pipe of length L (also equal to height difference h). In most textbooks and articles I've seen they use the normal stack effect, i.e. the pressure difference = (rhoambient - rhoout)*g*height. This is also equal the weight difference between the air column in the pipe and the same volume of air column at the ambient temperature, IF it is assumed that the temperature in the pipe is constant and equal to Tout. This is typical of a stack/chimney where hot gas enters at the inlet and the temperature stays constant, assuming adiabatic walls. In terms of buoyancy forces it makes sense to me that the pressure difference is analogous to the weight difference between the air column in the pipe and an equivalent ambient air column.
HOWEVER, when ambient air enters the pipe and is progressively heated as it travels upwards, the weight of this air column will be less than the air column described above, where hot gas enters the pipe, thus, the pressure differential should be less?
I've seen one article where they've used a temperature profile factor ,which they said is 0.5 for a linear temperature profile. This makes sense to me. Is my thinking correct or am I missing something?
Consider a vertical pipe of length L (also equal to height difference h). In most textbooks and articles I've seen they use the normal stack effect, i.e. the pressure difference = (rhoambient - rhoout)*g*height. This is also equal the weight difference between the air column in the pipe and the same volume of air column at the ambient temperature, IF it is assumed that the temperature in the pipe is constant and equal to Tout. This is typical of a stack/chimney where hot gas enters at the inlet and the temperature stays constant, assuming adiabatic walls. In terms of buoyancy forces it makes sense to me that the pressure difference is analogous to the weight difference between the air column in the pipe and an equivalent ambient air column.
HOWEVER, when ambient air enters the pipe and is progressively heated as it travels upwards, the weight of this air column will be less than the air column described above, where hot gas enters the pipe, thus, the pressure differential should be less?
I've seen one article where they've used a temperature profile factor ,which they said is 0.5 for a linear temperature profile. This makes sense to me. Is my thinking correct or am I missing something?