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- W1489923218 abstract "The purpose of this study on micro-vane secondary flow control is to demonstrate the viability and economy of Response Surface Methodology (RSM) to optimally design micro-vane secondary flow control arrays, and to establish that the aeromechanical effects of engine face distortion can also be included in the design and optimization process. These statistical design concepts were used to investigate the design characteristics of unit strength micro-effector arrays. Low unit strength micro-effectors are micro-vanes set at very low angles-of-incidence with very long chord lengths. They were designed to influence the near wall inlet flow over an extended streamwise distance, and their advantage lies in low total pressure loss and high effectiveness in managing engine face distortion. Therefore, this report examines optimal micro-vane secondary flow control array designs for compact inlets through a Response Surface Methodology." @default.
- W1489923218 created "2016-06-24" @default.
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- W1489923218 date "2013-07-31" @default.
- W1489923218 modified "2023-09-23" @default.
- W1489923218 title "Optimal Micro-Vane Flow Control for Compact Air Vehicle Inlets" @default.
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- W1489923218 hasPublicationYear "2013" @default.
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