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Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. 5 - Performance of two tangential jet blades

机译：高负荷涡轮定子叶片环形叶栅扇区的试验研究。 5 - 两个切向喷射叶片的性能

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Testing low reaction jet turbine stator blades in six-blade annular cascade

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作者
Bettner, J. L.;
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年度 1970
页码 1-167
总页数 167
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; CASCADE FLOW; STATOR BLADES; TURBINE BLADES; ANNULAR FLOW; FLOW VELOCITY;

机译：空气动力学特征;级联流程;定子刀片; TURBINE BLaDEs;环形流动;流量速度;
入库时间 2022-08-29 11:13:45

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1. Blade Bowing Effect on Aerodynamic Performance of a Highly Loaded Turbine Cascade [J] . Chunqing Tan, Hualiang Zhang, Hongde Xia, Journal of propulsion and power . 2010,第3期

机译：叶片弯曲对高负荷涡轮叶栅气动性能的影响
2. Blade Bowing Effect on Aerodynamic Performance of a Highly Loaded Turbine Cascade [J] . Chunqing Tan∗ Hualiang Zhang† Hongde Xia‡ and Haisheng Chen§Atsumasa Yamamoto¶ Journal of Propulsion and Power . 2010,第3期

机译：叶片弯曲对高负荷涡轮叶栅气动性能的影响
3. Experimental Investigation of Endwall and Suction Side Blowing in a Highly Loaded Compressor Stator Cascade [J] . Daniel Nerger, Horst Saathoff, Rolf Radespiel, Journal of turbomachinery . 2012,第2期

机译：高负荷压气机定子叶栅端壁和吸风侧吹的实验研究
4. NUMERICAL INVESTIGATION OF BLADE PROFILE EFFECTS ON AERODYNAMIC PERFORMANCE OF ULTRA-HIGHLY LOADED TURBINE CASCADES [C] . Hoshio Tsujita, Shimpei Mizuki, Atsumasa Yamamoto American Society of Mechanical Engineers(ASME) Turbo Expo vol.5 pt.B; 20040614-17; Vienna(AT) . 2004

机译：叶片轮廓对超大负荷涡轮叶栅气动性能的数值研究
5. Experimental investigation of secondary flows in a family of three highly loaded low-pressure turbine cascades. [D] . Zoric, Tatjana. 2006

机译：三个高负荷低压涡轮机叶栅系列中二次流的实验研究。
6. Experimental investigation of secondary flows in a family of three highly loaded low-pressure turbine cascades [O] . Tatjana Zorić -1

机译：三家高负荷低压涡轮机级联家族中二次流动的实验研究
7. Experimental Investigation in an Annular Cascade Sector of Highly Loaded Turbine Stator Blading. 5 - Performance of Two Tangential Jet Blades [R] . Bettner, J. L. 1970

机译：高负荷涡轮定子叶片环形叶栅扇区的试验研究。 5 - 两个切向喷射叶片的性能

Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. 5 - Performance of two tangential jet blades

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