Author:
Camac Morton,Feinberg Robert M.
Abstract
An infra-red heat-transfer gauge was used in a shock tube for end-wall measurements of the convective heat transfer from argon behind the reflected shock. The thermal conductivity of neutral (un-ionized) argon was measured before the ionization-relaxation time, and was fitted with the power-law temperature dependence 4·2 × 10−5(T/300)0·76±0·03cal/sec cm°K, whereTis measured in °K, and ±0·03 refers to the probable error The free-stream temperature ranged from 20,000 to 75,000°K, corresponding to incident-shock velocities from 3 to 6mm/μsec. At later times, after the free stream established equilibrium ionization, the convective-heat-transfer rate remained the same as the initial rate with neutral argon. Theoretical predictions of Fay & Kemp (1965), assuming equilibrium-boundary-layer conditions, are 20–30% below the experimental values. Also reported in this paper are measurements of the ionization times behind the reflected shock, and these are in agreement with an extrapolation of the Petschek & Byron (1957) measurements behind the incident shock. There is a discussion of the large changes in the gas conditions behind the reflected shock due to the ionization process. The final equilibrium conditions are reached abruptly, as indicated by the continuum-radiation emission which becomes constant immediately after ionization relaxation.
Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference18 articles.
1. Sturtevant, B. 1964 APS Bull. 9,583.
2. Reilly, J. P. 1963 Master of Aeronautical Engineering Thesis, Mass. Inst. Tech.
3. Fay, J. A. 1964 The High Temperature Aspects of Hypersonic Flow ,p.583,ed. W. C. Nelson .London:Pergamon Press.
4. Mies, F. H. 1962 J. Chem. Phys. 37,1101.
5. Petschek, H. E. , Rose, P. H. , Glick, H. S. , Kane, A. & Kantrowitz, A. R. 1955 J. Appl. Phys. 26,83.
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