Capturing transition features around a wing by reduced-order modeling based on compressible Navier–Stokes equations
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Publication:5304809
DOI10.1063/1.3234398zbMath1183.76108OpenAlexW1966011011MaRDI QIDQ5304809
Rémi Bourguet, Marianna Braza, A. Bouhadji, A. Sevrain
Publication date: 18 March 2010
Published in: Physics of Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1063/1.3234398
Navier-Stokes equationsMach numbercompressible flowflow simulationaerodynamicsflow instabilityaerospace components
Related Items (4)
Streamwise vortices, cellular shedding and force coefficients on finite wing at low Reynolds number ⋮ Calibration of projection-based reduced-order models for unsteady compressible flows ⋮ Reduced-order modeling of transonic flows around an airfoil submitted to small deformations ⋮ Data-driven closure of projection-based reduced order models for unsteady compressible flows
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