design, analysis and optimization of the ejector injection nozzle supersonic wind tunnel
نویسندگان
چکیده
in this article, an algorithm for designing of a supersonic wind tunnel injection nozzle ejector is presented and based on this algorithm, a new ejector is designed for a supersonic wind tunnel. the injection nozzle consists of a volute, a nozzle, and several vanes. designed injection nozzle is simulated numerically, and the results are compared with the present injection nozzle. the results show the efficiency in the designed version is higher about 2.1%. besides, the flow uniformity of the new injection nozzle is better and other are occurred in it. scale-up and mapping the pre designed aerodynamic curves with inverse design method, and use it for other similar cases is one of the innovations of this article.
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عنوان ژورنال:
مکانیک سیالات و آیرودینامیکجلد ۲، شماره ۴، صفحات ۰-۰
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