Resistance Thermometer for Heat Transfer Measurements in a Shock Tube
- Creators
- Rabinowicz, J.
- Jessey, M. E.
- Bartsch, C. A.
Abstract
This report describes a method for the application of the well-known principle of the resistance thermometer to the problem of measuring surface temperatures and heat transfer rates under highly transient conditions, such as are experienced in a shock tube. By using a thin platinum film sputtered on glass, a resistance thermometer gage is obtained which has a response lag of less than 1 µ sec, a linear output of 2-3 mv/°c, repeatability and durability. The gage preparation, including the sputtering technique, calibration method, and response characteristics are discussed, and some measurements of surface temperatures and heat transfer rates on models in the shock tube are presented in order to illustrate the performance that can be expected from this instrument.
Additional Information
ARMY ORDNANCE CONTRACT NO. DA-04-495-Ord-19 Army Project No. 5B0306004 Ordnance Project No. TB3-0118 OOR Project No. 1600-PE.Attached Files
Submitted - Resistance_Thermometer_for_Heat_Transfer_Measurement_in_a_Shock_tube.pdf
Files
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md5:c5cd2bd49211282c923ca3692f063c99
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Additional details
- Eprint ID
- 62668
- Resolver ID
- CaltechAUTHORS:20151207-161105278
- U.S. Army Office of Ordnance
- DA-04-495-Ord-19
- Created
-
2015-12-08Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Hypersonic Research Project
- Series Name
- Hypersonic Research Project Memorandum
- Series Volume or Issue Number
- 33