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机构地区:[1]中国科学院工程热物理研究所,100080 [2]北京航空航天大学
出 处:《航空动力学报》1993年第2期177-178,共2页Journal of Aerospace Power
基 金:航空科学基金资助研究课题
摘 要:An extremely simple,rapid and universal turbine cascade design program is develope d for contra rotating turbine cascades.With its simplest operating condition,only four data are necessary to be input for obtaining the geometry of a good enough cascade.They are just the input data for designing a cascade-the inlet Mach number and flow angle,the outlet Mach number and the specific heat ratio of working substance.Therefor e,it means that the design can be accomplished without any additiona l human decision.The program is based on the Mean-Stream-Line Method .It is given in detail how to select the independent design functions of this method in programming.This program enables to be operated with a very small computer,even a pocket computer such as the Sharp PC 1500.An extremely simple,rapid and universal turbine cascade design program is develope d for contra rotating turbine cascades.With its simplest operating condition,only four data are necessary to be input for obtaining the geometry of a good enough cascade.They are just the input data for designing a cascade-the inlet Mach number and flow angle,the outlet Mach number and the specific heat ratio of working substance.Therefor e,it means that the design can be accomplished without any additiona l human decision.The program is based on the Mean-Stream-Line Method .It is given in detail how to select the independent design functions of this method in programming.This program enables to be operated with a very small computer,even a pocket computer such as the Sharp PC 1500.
分 类 号:V232.4[航空宇航科学与技术—航空宇航推进理论与工程]
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