Gas turbine aerodynamics present modern engineering challenges, especially at high speeds where flow can reach transonic regimes, inducing complex aerodynamic phenomena like boundary-layer separation and shock-wave/boundary-layer interactions.
Towards Novel Physical Understanding of Gas Turbine Aerothermodynamics with Wall-Modeled LES and Immersed Boundary Method
De Vanna F.
;Benini E.
2026
Abstract
Gas turbine aerodynamics present modern engineering challenges, especially at high speeds where flow can reach transonic regimes, inducing complex aerodynamic phenomena like boundary-layer separation and shock-wave/boundary-layer interactions.
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