IGTC-41 CRITICAL ASSESSMENT OF THERMOPHYSICAL PROPERTIES DATA OF COMBUSTION GASES FOR CALCULATING THE PERFORMANCE OF GAS TURBINE(Session A-12 Cycle Performance)
スポンサーリンク
概要
- 論文の詳細を見る
A consistent set of simple equations of the thermodynamic and transport properties of the combustion products have been developed for gas turbine calculations based on the critically evaluated data and on the recent theory. The properties considered are, the density, the heat capacity at constant pressure, the enthalpy, the entropy, the viscosity and the thermal conductivity. The properties of the combustion products of various fuel at various air/fuel ratios can be calculated using these equations. The temperature and pressure ranges are up to 2000K and up to 10MPa.
- 公益社団法人日本ガスタービン学会の論文
著者
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HOSHINO T.
Department of Pedodontics
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Hoshino T
Shizuoka Univ. Hamamatsu Jpn
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Matsunaga N.
Department of Mechanical Engineering, Keio University
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Nagashima A.
Department of Mechanical Engineering, Keio University
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Nagashima A.
Department Of Mechanical Engineering Keio University
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Hoshino T.
Department Of Pediatric Dentistry Osaka University Graduate School Of Dentistry
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Hoshino T.
Department of Animal Husbandry, Faculty of Agriculture, Tohoku University
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