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Strain Gage Thermal Output
and Gage Factor Variation with Temperature

Compensation for Thermal Output -
Self-Temperature-Compensated Gages

The metallurgical properties of certain strain gage alloys - in particular, constantan and modified Karma (Micro-Measurements A and K alloys, respectively) - are such that these alloys can be processed to minimize the thermal output over a wide temperature range when bonded to test materials with thermal expansion coefficients for which they are intended. Strain gages employing these specially processed alloys are referred to as self-temperature-compensated .

3-Wire Circuit
Since the advent of the self-temperature-compensated strain gage, the requirement for a matching unstrained dummy gage in the adjacent arm of the Wheatstone bridge has been relaxed considerably. It is now normal practice when making strain measurements at or near room temperature to use a single self-temperature-compensated gage in a quarter-bridge arrangement (with a three-wire hookup), completing the bridge circuit with a stable fixed resistor in the adjacent arm (Fig. 3). Such "bridge-completion" resistors, with very low temperature coefficients of resistance, are supplied by Micro-Measurements and are incorporated in most modern strain indicators.



Fig.3 - A single self-temperature-compensated strain gage in a 3-wire quarter-bridge circuit exemplifies modern strain gage practice for stress analysis measurements.

Characteristics of Compensated Gages
Figure 4 illustrates the thermal output characteristics of typical A- and K- alloy self-temperature-compensated strain gages. As demonstrated by the figure, the gages are designed to minimize the thermal output over the temperature range from about 0° to +400° F (-20° to +205° C). When the self-temperature-compensated strain gage is bonded to a material having the thermal expansion coefficient for which the gage is intended, and when operated within the temperature range of effective compensation, strain measurements can often be made without the necessity of correcting for thermal output. If correction for thermal output is needed, it can be made as shown in the following sections.


Fig.4 - Typical thermal output variation with temperature for self-temperature-compensated constantan (A-alloy) and modified Karma (K-alloy) strain gages.

Self-temperature-compensated strain gages can also be used in the manner described previously . That is, when circumstances are such that a pair of matched gages can be used in adjacent arms of the bridge circuit, with both gages maintained at the same temperature, and with one of the gages unstrained (or strained at a determinate ratio to the other gage), excellent temperature compensation can be achieved over a wide temperature range.

S-T-C Number
The designations of Micro-Measurements self-temperature-compensated strain gages include a two-digit S-T-C number identifying the nominal thermal expansion coefficient (in ppm/° F) of the material on which the gage will exhibit optimum thermal output characteristics as shown in Fig. 4. Micro-Measurements constantan alloy gages are available in the following S-T-C numbers: 00, 03, 05, 06, 09, 13, 15, 18, 30, 40, and 50. S-T-C numbers of 30 and higher are intended primarily for use on plastics. In K alloy, the range of S-T-C numbers is more limited, and consists of 00, 03, 05, 06, 09, 13, and 15. For reference convenience, a table lists a number of engineering materials, and gives nominal values of the Fahrenheit and Celsius expansion coefficients for each, along with the S-T-C number which would normally be selected for strain measurements on that material. The table also identifies those test materials used in determining the published thermal output curves for Micro-Measurements self-temperature-compensated strain gages.

If a strain gage with a particular S-T-C number is installed on a material with a nonmatching coefficient of expansion, the thermal output characteristics will be altered from those shown in Fig. 4 by a general rotation of the curve about the room-temperature reference point. When the S-T-C number is lower than the material expansion coefficient, the rotation is counterclockwise; and when higher, clockwise. Rotation of the thermal output curve by intentionally mismatching the S-T-C number and expansion coefficient can be used to bias the thermal output characteristics so as to favor a particular working temperature range.



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