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An "Inefficient Fin" Non-Dimensional Parameter to Measure Gas Temperatures EfficientlyA gas containment vessel that is not in thermal equilibrium with the bulk gas can affect its temperature measurement. The physical nature of many gas dynamics experiments often makes the accurate measurement of temperature a challenge. The environment itself typically requires that the thermocouple be sheathed, both to protect the wires and hot junction of the instrument from their environment, and to provide a smooth, rigid surface for pressure sealing of the enclosure. However, that enclosure may also be much colder than the gas to be sensed, or vice-versa. Either way, the effect of such gradients is to potentially skew the temperature measurements themselves, since heat may then be conducted by the instrument. Thermocouple designers traditionally address this problem by insulating the sheath from the thermocouple leads and hot junction as much as possible. The thermocouple leads are typically packed in a ceramic powder inside the sheath, protecting them somewhat from temperature gradients along the sheath, but there is no effective mechanism to shield the sheath from the enclosure body itself. Standard practice dictates that thermocouples be used in installations that do not present large thermal gradients along the probe. If this conduction dominates heat transfer near the tip of the probe, then temperature measurements may be expected to be skewed. While the same problem may be experienced in the measurement of temperature at various points within a solid in a gradient, it tends to be aggravated in the measurements of gas temperature, since heat transfer dependent on convection is often less efficient than conduction along the thermocouple. The proposed solution is an inefficient fin thermocouple probe. Conventional wisdom suggests that in many experiments where gas flows through an enclosure (e.g., flow in pipe, manifold, nozzle, etc.), the thermocouple be introduced flush to the surface, so as not to interfere with the flow. In practice, however, many such experiments take place where the flow is already turbulent, so that a protruding thermocouple probe has a negligible effect on the flow characteristics. The key question then becomes just how far into the flow should a thermocouple protrude in order to properly sense the gas temperature at that point. Modeling the thermocouple as an "inefficient fin" directly addresses this question. The appropriate assumptions in this case are: one-dimensional conduction along the fin; steady-state, constant, and homogeneous thermal conductivity; negligible radiation; and a uniform, constant heat transfer coefficient over the probe surface. It is noted that the nature of the ceramic-filled probe makes the key assumption of homogeneous thermal conductivity that much more conservative.
Document ID
20120009251
Acquisition Source
Armstrong Flight Research Center
Document Type
Other - NASA Tech Brief
Authors
Lemieux, Patrick
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Murray, William
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Cooke, Terry
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Gerhardt, James
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2012
Publication Information
Publication: NASA Tech Briefs, May 2012
Subject Category
Man/System Technology And Life Support
Report/Patent Number
DRC-010-030
Distribution Limits
Public
Copyright
Public Use Permitted.
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