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- W2095280980 abstract "The principles of aircraft thermometer design are reviewed, from which it is deduced that the conical head design possesses distinct advantages over other kinds of thermometer head in high-speed flight. The construction of the thermometer is described and the results of wind-tunnel tests are quoted and discussed. The lag and radiation errors are calculated and the extension of the use of the thermometer to supersonic flight is discussed. An outstanding feature of this thermometer is the remarkable constancy of the recovery factor over a range of Mach numbers from 0.2 to 0.9 and its rapid response to temperature changes, the lag coefficient being of the order of 2 s." @default.
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- W2095280980 date "1958-12-01" @default.
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- W2095280980 title "A thermometer for high-speed aircraft" @default.
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- W2095280980 doi "https://doi.org/10.1088/0950-7671/35/12/301" @default.
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