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Variations in Upstream Vane Loading With Changes in Back Pressure in a Transonic Compressor

机译：跨音速压缩机中背压变化的上游叶片加载的变化

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Douglas P. Probasco; J. Mitch Wolff; William W. Copenhaver; Randall M. Chriss;
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年度 1998
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1. Axial spacing effects in a transonic compressor on the upstream vane loading [J] . Douglas P. Probasco, J. Mitch Wolff, William W. Copenhaver, International Journal of Turbo and Jet Engines . 2000,第3期

机译：跨音速压缩机的轴向间距对上游叶片载荷的影响
2. Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part Ⅱ: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall [J] . Harika S. Kahveci, Charles W. Haldeman, Randall M. Mathison, Journal of turbomachinery . 2013,第2期

机译：1-1 / 2级高压跨音速涡轮的薄膜冷却叶片的传热-第二部分：冷却变化对叶片翼型和内端壁的影响
3. Numerical evaluation of transient flow characteristics in a transonic centrifugal compressor with vaned diffuser [J] . Zamiri Ali, Lee Byung Ju, Chung Jin Taek Aerospace science and technology . 2017,第nova期

机译：带叶片扩压器的跨音速离心压缩机瞬态流动特性的数值评估
4. HEAT TRANSFER FOR THE FILM-COOLED VANE OF A 1-1/2 STAGE HIGH- PRESSURE TRANSONIC TURBINE - PART Ⅱ: EFFECT OF COOLING VARIATION ON THE VANE AIRFOIL AND INNER ENDWALL [C] . Harika S. Kahveci, Charles W. Haldeman, Randall M. Mathison, ASME turbo expo . 2012

机译：1-1 / 2级高压超音速涡轮机的膜冷风的传热-第二部分：冷却变化对叶片翼型和内壁的影响
5. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor [D] . Heberling, Brian. 2017

机译：自激叶尖流动不稳定性和上游叶片行相互作用对跨音速压缩机性能预测影响的数值分析
6. Variations in Battery Life of a Heart—Lung Machine Using Different Pump Speeds Pressure Loads Boot Material Centrifugal Pump Head Multiple Pump Usage and Battery Age [O] . Cornelius Marshall, Martin Hargrove, Aonghus O’Donnell, 2005

机译：使用不同的泵速压力载荷保护罩材料离心泵压头多次使用泵和电池寿命的心肺机电池寿命的变化
7. Transonic Compressor Influences on Upstream Surface Pressures With Axial Spacing [O] . Peter J. Koch, Douglas P. Probasco, J. Mitch Wolff, 1999

机译：跨音速压缩机对轴向间距的上游表面压力影响

Variations in Upstream Vane Loading With Changes in Back Pressure in a Transonic Compressor

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