Stochastic boundary condition effects on supersonic leading edge blowing

DOI10.1016/J.COMPFLUID.2022.105513OpenAlexW4281479673MaRDI QIDQ2158170

Francisco Lozano, Guillermo Paniagua, Iman Rahbari, Guang Lin

Publication date: 22 July 2022

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2022.105513

zbMATH Keywords

supersonic flowflow controlpolynomial chaosbow shockbbow shockCoandafflow control

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

• Unnamed Item
• Padé-Legendre approximants for uncertainty analysis with discontinuous response surfaces
• Effects of blunt trailing edge flow discharge in supersonic regime
• Some physical aspects of shock wave/boundary layer interactions
• Turbulent flow through a plane sudden expansion of modest aspect ratio
• Uncertainty Quantification and Polynomial Chaos Techniques in Computational Fluid Dynamics
• Uncertainty propagation in CFD using polynomial chaos decomposition
• Shock Wave Drag Reduction

This page was built for publication: Stochastic boundary condition effects on supersonic leading edge blowing