Published January 1956
| Published
Journal Article
Open
Resistance Thermometer for Transient High-Temperature Studies
- Creators
- Rabinowicz, J.
- Jessey, M. E.
- Bartsch, C. A.
Chicago
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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.
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.Attached Files
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Additional details
- Eprint ID
- 86696
- Resolver ID
- CaltechAUTHORS:20180529-163723729
- U.S. Army Office of Ordnance
- DA-04-495-Ord-19
- Air Force Office of Scientific Research (AFOSR)
- Created
-
2018-05-30Created from EPrint's datestamp field
- Updated
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2021-11-15Created from EPrint's last_modified field
- Caltech groups
- GALCIT