Markus Zauner
Markus Zauner
Verified email at soton.ac.uk - Homepage
Title
Cited by
Cited by
Year
Direct numerical simulations of transonic flow around an airfoil at moderate Reynolds numbers
M Zauner, N De Tullio, ND Sandham
AIAA Journal 57 (2), 597-607, 2018
122018
Linear Stability Prediction of Vortex Structures on High Pressure Turbine Blades
M Zauner, ND Sandham, APS Wheeler, RD Sandberg
International Journal of Turbomachinery, Propulsion and Power 2 (2), 8, 2017
122017
An error indicator for finite difference methods using spectral techniques with application to aerofoil simulation
CT Jacobs, M Zauner, N De Tullio, SP Jammy, DJ Lusher, ND Sandham
Computers & Fluids 168, 67-72, 2018
92018
Grid refinement using spectral error indicators with application to airfoil DNS
M Zauner, CT Jacobs, N Sandham
52018
Unsteady behaviour in direct numerical solutions of transonic flow around an airfoil.
M Zauner, N De Tullio, N Sandham
2018 Fluid Dynamics Conference, 2911, 2018
52018
Direct numerical simulation and stability analysis of transonic flow around airfoils at moderate Reynolds numbers
M Zauner
University of Southampton, 2019
32019
LES study of the three-dimensional behaviour of unswept wing sections at buffet conditions
M Zauner, ND Sandham
ERCOFTAC Workshop Direct and Large Eddy Simulation, 329-334, 2019
22019
Multiblock structured grids for direct numerical simulations of transonic wing sections
M Zauner, ND Sandham
Proceedings of the Tenth International Conference on Computational Fluid …, 2018
22018
Modal Analysis of a Laminar-Flow Airfoil under Buffet Conditions at Re= 500,000
M Zauner, ND Sandham
Flow, Turbulence and Combustion, 1-24, 2019
12019
Wide domain simulations of flow over an unswept laminar wing section undergoing transonic buffet
M Zauner, ND Sandham
Physical Review Fluids 5 (8), 083903, 2020
2020
Dataset for modal analysis of a laminar-flow airfoil under buffet conditions at Re= 500,000
M Zauner, N Sandham
University of Southampton, 2019
2019
Incipient buffet over laminar-flow airfoil-a DNS study at moderate Reynolds numbers
M Zauner, N Sandham
2018
Dataset for direct numerical simulations of a transonic airfoil at a Reynolds number of Re= 500,000
M Zauner, N Sandham, N De Tullio
University of Southampton, 2018
2018
Error severity values from simulations of a Taylor-Green vortex and a V2C aerofoil, computed using an error indicator
CT Jacobs, M Zauner, N De Tullio, S Jammy, D Lusher, N Sandham
University of Southampton, 2018
2018
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