scb wing optimization component (ONERA The French Aerospace Lab)
90
Structured Review
ONERA The French Aerospace Lab
scb wing optimization component
Scb Wing Optimization Component, supplied by ONERA The French Aerospace Lab, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
https://www.bioz.com/product/scb+wing+optimization+component/scb+wing+optimization+component/10__1080_slash_17797179__2017__1386022-56-21-8
Average 90 stars, based on 1 article reviews
Scb Wing Optimization Component, supplied by ONERA The French Aerospace Lab, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
https://www.bioz.com/product/scb+wing+optimization+component/scb+wing+optimization+component/10__1080_slash_17797179__2017__1386022-56-21-8
Average 90 stars, based on 1 article reviews
scb wing optimization component - by Bioz Stars,
2026-09
90/100 stars
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other:Article Title: Application of the adjoint optimisation of shock control bump for ONERA-M6 wing Article Snippet: This article is devoted to the numerical investigation of the shock wave/boundary layer interaction (SWBLI) as the main factor influencing the aerodynamic performance of transonic bumped airfoils and wings.. The numerical analysis is conducted for the ONERA-M6 wing through a shock control bump (SCB) shape optimisation process using the adjoint optimisation method.. SWBLI is analyzed for both clean and bumped airfoils and wings, and it is shown how the modified wave structure originating from upstream of the SCB reduces the wave drag, by improving the boundary layer velocity profile downstream of the shock wave. |