An apparent anomaly was resolved and a
correction was devised.
advertisement:
A computational-simulation study of the flow of air
through a thermo-anemometer chamber was performed
to resolve what originally seemed to be an anomaly in the
measurement data obtained by use of the chamber. The
thermo-anemometer chamber is a test chamber used to
measure the rate of generation of heat by a device placed
within it. In the original application that produced the
apparent anomaly that prompted this study, the chamber
was used to measure the power dissipation (as manifested by
heating) in an operating power-supply inductor. The apparent
anomaly was that the heating of the inductor as calculated
from the measurements made by use of the chamber
seemed unrealistically high.
Figure 1. The Thermo-Anemometer Chamber is an instrumented box equipped with an inlet blower and with instrumentation for measuring inlet temperature and outlet temperature and airflow speed. This is a simplified view representative of the computational model used to simulate the air flow in the chamber.
The thermo-anemometer chamber (see Figure 1)
includes a thermally insulating box with inlet and outlet
holes. A blower at the inlet forces air through the box.
There are a thermo-anemometer and a thermometer at the
outlet and a thermometer at the inlet. In principle, the rate
of generation of heat by a power-supply inductor or other
device in the chamber can be calculated from the outlet
area, the outlet air speed (as measured by the thermoanemometer),
the barometric pressure, the relative humidity,
the inlet and outlet air temperatures, and the specific
heat of air and water vapor. For the purpose of computational
simulation, the chamber is deemed to be also
equipped with an outlet tube that serves to average the flow
somewhat and to help suppress vortices, which could be
problematic for interpretation of simulation data.
Figure 2. This Color-Coded Plot of Axial Velocity in a meridional plane at the outlet shows the effects of laminar flow at the outlet.
The simulation of airflow in the chamber was performed
by use of a computational fluid dynamics program called
COSMOSFlowWorks. As a compromise between avoiding
computational anomalies (necessitating a fine mesh) and
avoiding excessive computation time (necessitating a
coarse mesh), the chamber was divided into a computational
mesh of 48,000 cells. The inlet flow speed was assumed to
be constant at 5.1 m/s. Computations were performed for a series of outlet diameters ranging from 2 to 4" (5.08 to
10.16 cm).
The simulation results revealed the source of the apparent
anomaly to be a combination of Bernoulli-like and laminar-flow
effects at the outlet. For example, in Figure 2, which
depicts results for the case in which the inlet and outlet diameters
are both 3" (7.62 cm), the axial velocity at the edge of the
outlet is reduced and the axial velocity in the center of the outlet
exceeds the inlet velocity; the effect on the axial velocity
averaged across the outlet area is equivalent to that of reducing
the outlet diameter. This effect causes the thermoanemometer,
located in the center of the outlet, to read a
speed greater than the cross-sectional average, so that the use
of this speed in estimating the heat-dissipation rate gives rise to
an unrealistically high value. The simulation results make it
possible to calculate an effective reduced diameter of the outlet
port to correct the apparent anomaly.
This work was done by Gregory K. Ovrebo of the Army Research
Laboratory.
ARL-0029
This Brief includes a Technical Support Package (TSP).
Simulation of Airflow Through a Test Chamber (reference ARL-0029) is currently available for download from the TSP library.
Subscribe today to receive the INSIDER, a FREE e-mail newsletter from NASA Tech Briefs featuring exclusive previews of upcoming articles, late breaking NASA and industry news, hot products and design ideas, links to online resources, and much more.