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TVT, 1991, Volume 29, Issue 3, Pages 515–520 (Mi tvt4247)  

Heat and Mass Transfer and Physical Gasdynamics

Modeling heat transfer during the flow of a hot gas past recesses in a shock tube

I. G. Zaltsman, A. A. Sokolskii, V. K. Shikov, E. B. Eigenson

Institute for High Temperatures, USSR Academy of Sciences

Abstract: An experimental study is made of heat transfer during the laminar flow of shockcompressed argon past recesses in the wall of a shock tube. It is shown that shock tubes can be used to model heat transfer during the steady flow of hot, fast-moving gases past recesses. Methodological problems that must be analyzed in the course of setting up specific experiments are also discussed. Data is obtained on the distribution of pressure and heat flux along the bottom of rectangular recesses for laminar subsonic and supersonic flows of shock-heated argon with shock-wave velocities of $1.5$$6$ km/sec and temperature factors up to $0.02$.

Full text: PDF file (437 kB)

English version:
High Temperature, 1991, 29:3, 406–410

Bibliographic databases:
UDC: 536.24
Received: 20.12.1989

Citation: I. G. Zaltsman, A. A. Sokolskii, V. K. Shikov, E. B. Eigenson, “Modeling heat transfer during the flow of a hot gas past recesses in a shock tube”, TVT, 29:3 (1991), 515–520; High Temperature, 29:3 (1991), 406–410

Citation in format AMSBIB
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\paper Modeling heat transfer during the flow of a hot gas past recesses in a shock tube
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\yr 1991
\vol 29
\issue 3
\pages 515--520
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\jour High Temperature
\yr 1991
\vol 29
\issue 3
\pages 406--410
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