34th Congress of the International Council of the Aeronautical Sciences

05 - Propulsion

GRADIENT-BASED OPTIMIZATION OF AN AXIAL COMPRESSOR UNDER INLET DISTORTION USING BODY-FORCE MODELING

C. Dosne¹, R. Barrier¹, S. Bourasseau¹, M. Carini¹, A. Dumont¹, J. Peter¹; ¹ONERA, France

An assessment of the body-force capabilities for axial compressor design under inlet distortion is proposed, using the novel adjoint body force tool recently implemented. Then, several optimizations - first under radial then under a full annulus BLI alike distortion - are conducted to demonstrate those capabilities, and to evaluate the adjoint body-force limitations.


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