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Heat waves in an electrothermal shock tube Armstrong, Bruce Allan
Abstract
The fluid flow in an electrothermal shock tube powered with a constant current was compared to that predicted by a heat wave model and found to be in qualitative agreement. An empirical heating characteristic, obtained experimentally from gas dynamical measurements, was verified with spectroscopic and velocity measurements indicating the flow is also in quantitative agreement with the model. Using a two step current pulse we launched double shock waves in argon with a subsonic heat wave. The interaction of these shock waves agreed very well with theory. Increasing the current in the second step created faster second shock waves until some limiting value of the current was reached, after which a second shock could no longer be produced. Rather, a supersonic heat wave was created which burned through the previously shock-compressed material. The velocities of the second shocks were in reasonable quantitative agreement with predictions of the heat wave theory, indicating again the flow in the shock tube is well described by the model. It was shown that the resulting fluid flow, after all the waves had interacted, did not depend on the history of the power pulse, only on its final magnitude.
Item Metadata
Title |
Heat waves in an electrothermal shock tube
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Creator | |
Publisher |
University of British Columbia
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Date Issued |
1978
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Description |
The fluid flow in an electrothermal shock tube powered with a constant current was compared to that predicted by a heat wave model and found to be in qualitative agreement. An empirical heating characteristic, obtained experimentally from gas dynamical measurements, was verified with spectroscopic and velocity measurements indicating the flow is also in quantitative agreement with the model. Using a two step current pulse we launched double shock waves in argon with a subsonic heat wave. The interaction of these shock waves agreed very well with theory. Increasing the current in the second step created faster second shock waves until some limiting value of the current was reached, after which a second shock could no longer be produced. Rather, a supersonic heat wave was created which burned through the previously shock-compressed material. The velocities of the second shocks were in reasonable quantitative agreement with predictions of the heat wave theory, indicating again the flow in the shock tube is well described by the model. It was shown that the resulting fluid flow, after all the waves had interacted, did not depend on the history of the power pulse, only on its final magnitude.
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Genre | |
Type | |
Language |
eng
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Date Available |
2010-02-26
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Provider |
Vancouver : University of British Columbia Library
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Rights |
For non-commercial purposes only, such as research, private study and education. Additional conditions apply, see Terms of Use https://open.library.ubc.ca/terms_of_use.
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DOI |
10.14288/1.0085512
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URI | |
Degree | |
Program | |
Affiliation | |
Degree Grantor |
University of British Columbia
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Campus | |
Scholarly Level |
Graduate
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Aggregated Source Repository |
DSpace
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Item Media
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Rights
For non-commercial purposes only, such as research, private study and education. Additional conditions apply, see Terms of Use https://open.library.ubc.ca/terms_of_use.