Delayed detached eddy simulations of fighter aircraft at high angle of attack

DOI10.1007/s10409-016-0565-3zbMath1361.76014OpenAlexW2405889965MaRDI QIDQ529172

Yong-Cai Geng, Sumit K. Garg

Publication date: 18 May 2017

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-016-0565-3

zbMATH Keywords

delayed detached eddy simulationmassively separationrealistic aircraft

Mathematics Subject Classification ID

Direct numerical and large eddy simulation of turbulence (76F65)

Related Items (2)

Density enhancement mechanism of upwind schemes for low Mach number flows ⋮ The secondary instabilities of stationary cross-flow vortices in a Mach 6 swept wing flow

Cites Work

• Computation of turbulent supersonic flows around pointed bodies having crossflow separation
• Approximate Riemann solvers, parameter vectors, and difference schemes
• A new version of detached-eddy simulation, resistant to ambiguous grid densities
• Numerical studies of flow over a circular cylinder at ReD=3900
• On the identification of a vortex
• Preconditioning applied to variable and constant density flows

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