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- W3120013623 abstract "As part of an effort to develop a parametric and coupled aero-propulsive conceptual design methodology for boundary layer ingesting (BLI) aircraft, there is a need to investigate propulsor sizing and off-design impacts on the ingested boundary layer. This study uses 3D CFD analysis to quantify the BLI effects trends as a function of fan annulus area and mass flow rate required, for engine locations similar to those on the the D8, NOVA-BLI and the STARC-ABL concepts. This study extends previous work that relied on CFD analysis of an axisymmetric model for the STARC-ABL concept. The results from this study highlight the propulsor’s contribution to the aero-propulsive coupling inherent in BLI concepts." @default.
- W3120013623 created "2021-01-18" @default.
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- W3120013623 date "2021-01-04" @default.
- W3120013623 modified "2023-09-27" @default.
- W3120013623 title "Assessment of Propulsor On-Design and Off-Design Impacts on BLI Effects" @default.
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- W3120013623 doi "https://doi.org/10.2514/6.2021-0605" @default.
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