Rabinowicz, J. and Jessey, M. E. and Bartsch, C. A. (1956) Resistance Thermometer for Transient High-Temperature Studies. Journal of Applied Physics, 27 (1). pp. 97-98. ISSN 0021-8979. doi:10.1063/1.1722210. https://resolver.caltech.edu/CaltechAUTHORS:20180529-163723729
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Abstract
Current interest in ultra-high-speed flight has stimulated the development of the shock tube as a device for simulating high stagnation temperatures in supersonic flow. The main difficulty in these tests is the extremely short duration of uniform flow, of the order of 100-500 µsec. This time interval dictates extremely fast response of any measuring instrument applied to shock tube research.
| Item Type: | Article | ||||||
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| Additional Information: | © 1956 The American Institute of Physics. (Received September 6, 1955) This work is part of a broad program of experimental and theoretical research on hypersonic and related flow problems sponsored jointly by the U. S. Army Ordnance and Air Force under Contract No. DA-04-495-Ord-19. | ||||||
| Group: | GALCIT | ||||||
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| Issue or Number: | 1 | ||||||
| DOI: | 10.1063/1.1722210 | ||||||
| Record Number: | CaltechAUTHORS:20180529-163723729 | ||||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20180529-163723729 | ||||||
| Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | ||||||
| ID Code: | 86696 | ||||||
| Collection: | CaltechAUTHORS | ||||||
| Deposited By: | George Porter | ||||||
| Deposited On: | 30 May 2018 15:01 | ||||||
| Last Modified: | 15 Nov 2021 20:41 |
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