Dr.-Ing. Markus Kloker

Dr.-Ing.
Markus J. Kloker
Leiter Transition und Turbulenz

Dieses Bild zeigt  Markus J. Kloker
Telefon0049 711 685-63427
Telefax0049 711 685-63438
E-Mail
Adresse
Universität Stuttgart
Institut für Aerodynamik und Gasdynamik
Pfaffenwaldring 21
D-70550 Stuttgart
Deutschland
Fachgebiet:

Main Research Topics

Spatial direct numerical simulation of flow instability - 3-d base flows
Stability theory with 1-d and 2-d eigenfunctions
Laminar-turbulent transition - laminar flow control - suction, blowing, roughness, plasma actuators
Disturbance receptivity and its control
Eco-Efficient Flight, Environmentally Responsible Aviation
Hypersonic boundary layers - 1.-mode/2.-mode/streak instabilities, roughness
Wall and film cooling in super-/hypersonic flow
Flow induced sound, sound control, and global instability
Active flow control


 

Inhaltsverzeichnis

  1. 2016-2020
  2. 2011-2015
  3. 2006-2010
  4. 1996-2000
  5. 1991-1995
  6. 1990

2016-2020

2017

DOERR, P.C., Kloker, M.J. (2017)
Crossflow transition control by upstream flow deformation using plasma actuators. J. Appl. Phys. 121, 063303 (2017),
http://dx.doi.org/10.1063/1.4975791.

2016

Keller, M., Kloker, M.J. (2016)
Direct numerical simulation of foreign-gas film cooling in supersonic boundary-layer flow. AIAA Journal 55, no. 1, 99-111;
http://arc.aiaa.org/doi/abs/10.2514/1.J055115.  

GROSKOPF, G., KLOKER, M.J. (2016)
Instability and transition mechanisms induced by skewed roughness elements in a high-speed boundary-layer. J. Fluid Mech. 805, 262-302, http://dx.doi.org/10.1017/jfm.2016.563.

DOERR, P.C., Kloker, M.J. (2016)
Transition control in a three-dimensional boundary layer by direct attenuation of nonlinear crossflow vortices using plasma actuators. Int. J. Heat Fluid Flow 61 (B), 449-465; 10.1016/j.ijheatfluidflow.2016.06.005.

KURZ, H.B.E., KLOKER, M.J. (2016)
Mechanisms of flow tripping by discrete roughness elements in a swept-wing boundary layer. J. Fluid Mech. 796, 158-194.

KURZ, H.B.E., KLOKER, M.J. (2016)
Receptivity of a swept-wing boundary layer to steady vortical free-stream disturbances. In: New Results in Numerical and Experimental Fluid Dynamics X (eds. A. Dillmann et al.), NNFM 132, peer-reviewed contributions to the 19. STAB/DGLR-Symposium, Munich, Nov. 2014, 227-236, Springer.

DOERR, P.C., Kloker, M.J. (2016)
Control of the secondary crossflow instability using plasma actuators. In: New Results in Numerical and Experimental Fluid Dynamics X (eds. A. Dillmann et al.), NNFM 132, peer-reviewed contributions to the 19. STAB/DGLR-Symposium, Munich, Nov. 2014, 101-111, Springer.

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