Welcome to the new version of CaltechAUTHORS. Login is currently restricted to library staff. If you notice any issues, please email coda@library.caltech.edu
Published January 1956 | Published
Journal Article Open

Resistance Thermometer for Transient High-Temperature Studies

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

Published - 1_2E1722210.pdf

Files

1_2E1722210.pdf
Files (350.8 kB)
Name Size Download all
md5:6271342d822e9e46a11c2755bcb3ae4b
350.8 kB Preview Download

Additional details

Created:
August 19, 2023
Modified:
October 18, 2023