Journal articles

Effect of pitch on the flow behavior around a hovering wing

S. Krishna; M. A. Green; K. Mulleners 

Experiments in Fluids. 2019-04-25. Vol. 60, num. 5, p. 60:86. DOI : 10.1007/s00348-019-2732-3.

Multiscale Vortex Characteristics of Dynamic Stall from Empirical Mode Decomposition

P. J. Ansell; K. Mulleners 

AIAA Journal. 2019.  p. 1-18. DOI : 10.2514/1.J057800.

Genetic Algorithm Based Optimization of Wing Rotation in Hover

A. Gehrke; G. Guyon-Crozier; K. Mulleners 

Fluids. 2018. Vol. 3, num. 3, p. 59. DOI : 10.3390/fluids3030059.

The role of surface vorticity during unsteady separation

M. S. Melius; K. Mulleners; R. B. Cal 

Physics of Fluids. 2018. Vol. 30, num. 4, p. 045108. DOI : 10.1063/1.5006527.

Cross-correlation analysis of synchronized PIV and microphone measurements of an oscillating airfoil

L. Siegel; K. Ehrenfried; C. Wagner; K. Mulleners; A. Henning 

Journal of Visualization. 2018. DOI : 10.1007/s12650-018-0473-7.

Flowfield and Force Evolution for a Symmetric Hovering Flat-Plate Wing

S. Krishna; M. Green; K. Mulleners 

AIAA Journal. 2018. Vol. 56, num. 4, p. 1360-1371. DOI : 10.2514/1.J056468.

Analysis of Intermittent Trailing-Edge Vortex Shedding Using Recurrence Plots

K. Mulleners; M. Ruetten 

AIAA Journal. 2017. Vol. 56, num. 2, p. 571-580. DOI : 10.2514/1.J056329.

Flow Development on a Flat-Plate Wing Subjected to a Streamwise Acceleration

K. Mulleners; P. Mancini; A. R. Jones 

AIAA Journal. 2017. Vol. 55, num. 6, p. 2118-2122. DOI : 10.2514/1.J055497.

Resulting Aerodynamic Losses of Combinations of Localized Roughness Patches on Turbine Blades

P. Gilge; K. Mulleners 

AIAA Journal. 2016. Vol. 54, num. 8, p. 2552-2555. DOI : 10.2514/1.J054602.

Dynamic stall of an experimental wind turbine blade

M. Melius; R. B. Cal; K. Mulleners 

Physics of Fluids. 2016. Vol. 28, num. 3, p. 034103. DOI : 10.1063/1.4942001.

Characterizing a burst leading-edge vortex on a rotating flat plate wing

A. R. Jones; A. Medina; H. Spooner; K. Mulleners 

Experiments in Fluids. 2016. Vol. 57, num. 4, p. 1-16. DOI : 10.1007/s00348-016-2143-7.

Impact of surface roughness on the turbulent wake flow of a turbine blade

K. Mulleners; P. Gilge; S. Hohenstein 

Journal of Aerodynamics. 2014. Vol. 2014, p. 458757. DOI : 10.1155/2014/458757.

Dynamic stall development

K. Mulleners; M. Raffel 

Experiments in fluids. 2013. Vol. 54, num. 2, p. 1-9. DOI : 10.1007/s00348-013-1469-7.

Dynamic stall control by passive disturbance generators

B. Heine; K. Mulleners; G. Joubert; M. Raffel 

AIAA journal. 2013. Vol. 51, num. 9, p. 2086-2097. DOI : 10.2514/1.J051525.

Dynamic stall on a fully equipped helicopter model

K. Mulleners; K. Kindler; M. Raffel 

Aerospace Science and Technology. 2012. Vol. 19, num. 1, p. 72-76. DOI : 10.1016/j.ast.2011.03.013.

The onset of dynamic stall revisited

K. Mulleners; M. Raffel 

Experiments in fluids. 2012. Vol. 52, num. 3, p. 779-793. DOI : 10.1007/s00348-011-1118-y.

Density tagging velocimetry

M. Raffel; R. Hernandez-Rivera; B. Heine; A. Schröder; K. Mulleners 

Experiments in fluids. 2011. Vol. 51, num. 2, p. 573-578. DOI : 10.1007/s00348-011-1058-6.

Aperiodicity in the near field of full-scale rotor blade tip vortices

K. Kindler; K. Mulleners; H. Richard; B. G. van der Wall; M. Raffel 

Experiments in fluids. 2011. Vol. 50, num. 6, p. 1601-1610. DOI : 10.1007/s00348-010-1016-8.

Impact of an invasive species, Crepidula fornicata, on the hydrodynamics and transport properties of the benthic boundary layer

F. Y. Moulin; K. Guizien; G. Thouzeau; G. Chapalain; K. Mulleners et al. 

Aquatic Living Resources. 2007. Vol. 20, num. 01, p. 15-31. DOI : 10.1051/alr:2007012.

Critical parameters for the partial coalescence of a droplet

T. Gilet; K. Mulleners; J-P. Lecomte; N. Vandewalle; S. Dorbolo 

Physical Review E. 2007. Vol. 75, num. 3, p. 036303. DOI : 10.1103/PhysRevE.75.036303.

Dancing droplets onto liquid surfaces

N. Vandewalle; D. Terwagne; K. Mulleners; T. Gilet; S. Dorbolo 

Physics of Fluids. 2006. Vol. 18, num. 9, p. 91106-91106. DOI : 10.1063/1.2335905.