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Quantification of the Effect of Circumferential Repeated 3D Features on Radial Displacement of a Compressor Casing Focusing Model Simplification: Part I

机译：定量圆周重复三维特征对压缩机壳体聚焦模型简化径向位移的影响：第一部分

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Tobias Schmidt; Volker Gümmer; Marco Konle;
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1. Uncertainty Quantification of Spalart-Allmaras Turbulence Model Coefficients for Simplified Compressor Flow Features [J] . He Xiao, Zhao Fanzhou, Vahdati Mehdi Journal of Fluids Engineering: Transactions of the ASME . 2020,第9期

机译：用于简化压缩机流动特征的Spalart-Allmaras湍流模型系数的不确定度量
2. Potential of surrogate modelling in compressor casing design focussing on rapid tip clearance assessments [J] . Schmidt T., Guemmer V., Konle M. The Aeronautical Journal . 2021,第1291期

机译：压缩机套管设计中替代模型的潜力焦点快速提示清关评估
3. Advanced Casing Design With Finite-Element Model of Effective Dogleg Severity, Radial Displacements, and Bending Loads [J] . A.R. McSpadden, O.D. Coker Ⅲ, G.C.Ruan SPE Drilling & Completion . 2012,第3期

机译：先进的套管设计，带有有效狗腿严重度，径向位移和弯曲载荷的有限元模型
4. NUMERICAL ANALYSIS OF FLOW IN A TRANSONIC COMPRESSOR WITH A SINGLE CIRCUMFERENTIAL CASING GROOVE: APPLICATION TO TWO DIFFERENT COMPRESSOR ROTORS [C] . Yasunori Sakuma, Toshinori Watanabe, Takeniro Himeno, ASME turbo expo: turbine technical conference and exposition . 2014

机译：单圆周壳体槽跨音速压缩机的流动数值分析：在两种不同压缩机转子上的应用
5. Tip clearance flow interaction with circumferential groove casing treatment in a transonic axial compressor [D] . Ross, Mark Hamilton 2014

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6. Radial and Circumferential Collagen Fibers Are a Feature of the Peripapillary Sclera of Human Monkey Pig Cow Goat and Sheep [O] . Alexandra Gogola, Ning-Jiun Jan, Kira L. Lathrop, -1

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7. Single and Multiple Circumferential Casing Groove for Stall Margin Improvement in a Transonic Axial Compressor [O] . A. F. Mustaffa, V. Kanjirakkad 2021

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8. Toward Optimum Configuration of Circumferential Groove Casing Treatment in Transonic Compressor Rotors [R] . Hah, C. 2011

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Quantification of the Effect of Circumferential Repeated 3D Features on Radial Displacement of a Compressor Casing Focusing Model Simplification: Part I

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