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INVESTIGATION OF A HIGHLY LOADED TWO-STAGE FAN-DRIVE TURBINE VOLUMEⅢ. PhaseⅡ, Part 2. Experimental Baseline Airfoil Evaluation

机译：高负荷两级风机涡轮增压量的研究Ⅲ。第二阶段，第2部分。实验基线翼型评估

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作者
H. Welna; D. E. Dahlberg; W. H. Heiser;
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年度 1969
页码 1-190
总页数 190
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Turbofan engines; Gas turbines; Blade airfoils; Boundary layer control; Gas turbine blades; Aerodynamic characteristics; Aerodynamics; Aircraft engines; Cascade structures; Two dimensional flow; Three dimensional flow;

机译：涡轮风扇发动机;燃气轮机;叶片翼型;边界层控制;燃气轮机叶片;空气动力学特性;空气动力学;飞机发动机;级联结构;二维流动;三维流动;

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7. Investigation of a Highly Loaded Two-Stage Fan-Drive Turbine. Volume I. Phase I. Preliminary Design Evaluation. [O] . Henry Welna, Donald E. Dahlberg, William H. Heiser 1969

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INVESTIGATION OF A HIGHLY LOADED TWO-STAGE FAN-DRIVE TURBINE VOLUMEⅢ. PhaseⅡ, Part 2. Experimental Baseline Airfoil Evaluation

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