دانلود مقاله ISI انگلیسی شماره 107220
ترجمه فارسی عنوان مقاله

تأثیر مکش لایه مرزی متحرک و تیغه بر روی میدان جریان و عملکرد آبشار افقی

عنوان انگلیسی
Influence of coupled boundary layer suction and bowed blade on flow field and performance of a diffusion cascade
کد مقاله سال انتشار تعداد صفحات مقاله انگلیسی
107220 2017 16 صفحه PDF
منبع

Publisher : Elsevier - Science Direct (الزویر - ساینس دایرکت)

Journal : Chinese Journal of Aeronautics, Volume 30, Issue 1, February 2017, Pages 249-263

ترجمه کلمات کلیدی
کمپرسور محوری مکش لایه مرزی، تیغه چاقو، جداسازی گوشه، روش متقابل، گرداب عبور
کلمات کلیدی انگلیسی
Axial compressor; Boundary layer suction; Bowed blade; Corner separation; Coupled method; Passage vortex;
پیش نمایش مقاله
پیش نمایش مقاله  تأثیر مکش لایه مرزی متحرک و تیغه بر روی میدان جریان و عملکرد آبشار افقی

چکیده انگلیسی

Results show that mid-span local boundary layer suction can effectively remove trailing edge separation, but deteriorate the flow fields near the endwall. The positive bowed cascade is beneficial for reducing open corner separation, but is detrimental to mid-span flow fields. The coupled method can further improve the performance and flow field of the cascade. The mid-span trailing edge separation and open corner separation are eliminated. Compared with linear cascade with suction, the coupled method reduces overall loss of the cascade by 31.4% at most. The mid-span loss of the cascade decreases as the suction coefficient increases, but increases as bow angle increases. The endwall loss increases as the suction coefficient increases. By contrast, the endwall loss decreases significantly as the bow angle increases. The endwall loss of coupled controlled cascade is higher than that of bowed cascade with the same bow angle because of the spanwise inverse “C” shaped static pressure distribution. Under different inlet boundary layer conditions, the coupled method can also improve the cascade effectively.