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Program for Aerodynamic Performance Tests of Helium Gas Compressor Model of the Gas Turbine High Temperature Reactor (GTHTR300)

机译：燃气轮机高温反应器氦气压缩机模型的空气动力学性能试验计划（GTHTR300）

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Shoji TAKADA; Takakazu TAKIZUKA; Kazuhiko KUNITOMI; Xing YAN; Masanori TANIHIRA; Hidehiko ITAKA; Eiji MORI;
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年度 2003
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2. A Review of the Turbine Cooling Fraction for Very High Turbine Entry Temperature Helium Gas Turbine Cycles for Generation IV Reactor Power Plants [J] . A. Gad-Briggs, P. Pilidis, T. Nikolaidis Journal of nuclear engineering and radiation science . 2017,第2期

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3. The effect of aspiration configuration on aerodynamic performance in compound lean compressor cascades of gas turbines [J] . Ding Jun, Wang Songtao, Xu Hao, Applied thermal engineering: Design, processes, equipment, economics . 2018,第期

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5. Investigation of a Novel Turbulence Model and Using Leading-Edge Slots for Improving the Aerodynamic Performance of Airfoils and Wind Turbines. [D] . Beyhaghi, Saman. 2017

机译：研究新型湍流模型并使用前沿槽改善机翼和风力涡轮机的空气动力学性能。
6. New steady-state microbial community compositions and process performances in biogas reactors induced by temperature disturbances [O] . Gang Luo, Davide De Francisci, Panagiotis G Kougias, 2015

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7. Feasibility Study on High Burnup Fuel for Gas Turbine High Temperature Reactor (GTHTR300), (II) [O] . Shoji KATANISHI, Masanobu TAKEI, Tetsuo NAKATA, 2004

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8. Investigations on an Experimental Air-Cooled Turbine Part Ⅲ.—the Effects of Cooling on the Overall Turbine Aerodynamic Performance and Initial Operation at an Inlet Gas Temperature of 140° deg K PartⅣ.—Examination of Sintered Vitallium Air-Cooled Turbine Blades Following 100 Hours' Operation at a Turbine Inlet Mean Gas Temperature of 1400 deg K [R] . N. E. WALDREN, C. J. HART, D. E. FRAY 1960

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Program for Aerodynamic Performance Tests of Helium Gas Compressor Model of the Gas Turbine High Temperature Reactor (GTHTR300)

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