Lift airfoils close to the airfoils in a flow with the maximum ``critical Mach numbers

DOI10.1134/s0015462822700057MaRDI QIDQ6169706

A. N. Kraĭko, V. A. Shapovalov

Publication date: 12 July 2023

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

genetic algorithmlift airfoils close to optimal ones with respect to highest critical Mach numberssegments of sonic streamlines approximated by Bernstein-Bézier curves

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

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• Shockless Design and Analysis of Transonic Cascade Shapes
• New Method for Designing Shock-Free Transonic Configurations
• Maximum critical Mach number flows around semi-infinite solids of revolution
• Calculation of Subsonic Cavities with Sonic Free Streamlines

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