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Showing 1 to 3 of 3 for “"Distortion transfer"”.
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Prediction of Inlet Distortion Transfer Through the Blade Rows in a Transonic Axial Compressor
… As previous research has shown total pressure distortion to be the dominant HCF driver in aero engines [Manwaring et al, 1997], an understanding of its transfer through, and impact on, subsequent turbomachine stages and engine components is an important topic for assessment. Since current …
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Performance of a boundary layer ingesting propulsion system
… body force approach to fan response to inlet distortion has been utilized to analyze the flow in the engine ducts. In addition to providing quantitative information as to the fuel burn benefit from BLI, the body force approach is also compared with two simpler analyses, one based on the …
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Use of Nonlinear Volterra Theory in Predicting the Propagation of Non-uniform Flow Through an Axial Compressor
… Previous research has shown total pressure distortions to be the dominant HCF driver in aero engines, and has demonstrated the damaging results of total pressure distortion induced HCF on first stage fan and compressor blade rows [Manwaring et al., 1997]. It is, however, also of interest to …