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- W1767502495 abstract "Aircraft have evolved into extremely complex systems that require adapted methodologies and tools for efficient design processes. A theoretical formulation based on exergy management is proposed for assessing the aerothermopropulsive performance of future aircraft configurations. The theoretical formulation has been numerically implemented in a FORTRAN code to postprocess Reynolds-averaged Navier–Stokes flow solutions. First, the exergy formulation is presented, and then the approach is applied to assess the performance of a simplified (two-dimensional) blended wing–body configuration with boundary-layer ingestion. The challenge of applying conventional drag/thrust bookkeeping is discussed, and the pertinence of the formulation is thereby reinforced. It is shown that this architecture wastes very little exergy in its wake/jet by exhibiting an exergy-waste coefficient lower than 3% in steady flight. Finally, heat transfer upstream of the propulsion system is found to yield an approximate 1.5% fuel saving. Overall, the benefit of the single-currency aspect of the exergy analysis is highlighted." @default.
- W1767502495 created "2016-06-24" @default.
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- W1767502495 date "2015-12-01" @default.
- W1767502495 modified "2023-10-01" @default.
- W1767502495 title "Exergy-Based Performance Assessment of a Blended Wing–Body with Boundary-Layer Ingestion" @default.
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- W1767502495 doi "https://doi.org/10.2514/1.j054072" @default.
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