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Featured researches published by Sina Kheirkhah.


Physics of Fluids | 2013

Turbulent premixed combustion in V-shaped flames: Characteristics of flame front

Sina Kheirkhah; Ömer L. Gülder

Flame front characteristics of turbulent premixed V-shaped flames were investigated experimentally using the Mie scattering and the particle image velocimetry techniques. The experiments were performed at mean streamwise exit velocities of 4.0, 6.2, and 8.6 m/s, along with fuel-air equivalence ratios of 0.7, 0.8, and 0.9. Effects of vertical distance from the flame-holder, mean streamwise exit velocity, and fuel-air equivalence ratio on statistics of the distance between the flame front and the vertical axis, flame brush thickness, flame front curvature, and angle between tangent to the flame front and the horizontal axis were studied. The results show that increasing the vertical distance from the flame-holder and the fuel-air equivalence ratio increase the mean and root-mean-square (RMS) of the distance between the flame front and the vertical axis; however, increasing the mean streamwise exit velocity decreases these statistics. Spectral analysis of the fluctuations of the flame front position depicts ...


Journal of Fluids Engineering-transactions of The Asme | 2013

Mitigation of Vortex-Induced Vibrations of a Pivoted Circular Cylinder Using an Adaptive Pendulum Tuned-Mass Damper

Sina Kheirkhah; Richard Lourenco; Serhiy Yarusevych; Sriram Narasimhan

A novel adaptive pendulum tuned-mass damper (TMD) was integrated with a two degree-of-freedom (DOF) cylindrical structure in order to control vortex-induced vibrations of the structure. The natural frequency of the TMD was adjusted autonomously in order to control the vortex-induced vibrations. The experiments were performed at a constant Reynolds number of 2100 and for four reduced velocities, 4.18, 5.44, 6.00, and 6.48. Two TMD damping ratios, 0 and 0.24, were investigated for a constant TMD mass ratio of 0.087. The results demonstrate that tuning the natural frequency of the TMD to the natural frequency of the structure decreases the amplitudes of transverse and streamwise vibrations of the structure significantly. Specifically, the transverse amplitudes of vibrations are decreased by a factor of ten and streamwise amplitudes of vibrations are decreased by a factor of three. Depending on the value of the TMD damping ratio, the frequency of transverse vibrations is either characterized by the natural frequency of the structure or by two other fundamental frequencies, one higher and the other lower than the natural frequency of the structure. The results demonstrate that, independent of the TMD damping and tuning frequency ratios, the frequency of streamwise vibrations matches that of the transverse vibrations in the synchronization region, and the cylinder traces elliptic trajectories. A mathematical model is proposed to gain insight into the frequency response of the structure and fluid-structure interactions. The model shows that, for low TMD damping ratios, the frequency response of the structure equipped with the TMD is characterized by two fundamental frequencies; whereas, for relatively high TMD damping ratios, the frequency response of the structure is characterized by a single frequency, i.e., the natural frequency. In both cases, the fluid forcing within the synchronization region is linked to the fundamental frequency/frequencies of the structure. Thus, the classical definition of synchronization applies to multiple DOF structures undergoing vortex-induced vibrations.


Combustion and Flame | 2015

Consumption speed and burning velocity in counter-gradient and gradient diffusion regimes of turbulent premixed combustion

Sina Kheirkhah; Ömer L. Gülder


Flow Turbulence and Combustion | 2014

Topology and Brush Thickness of Turbulent Premixed V-shaped Flames

Sina Kheirkhah; Ömer L. Gülder


Proceedings of the Combustion Institute | 2017

Non-stationary local thermoacoustic phase relationships in a gas turbine combustor

Sina Kheirkhah; B.D. Geraedts; Pankaj Saini; Krishna Venkatesan; Adam M. Steinberg


Combustion and Flame | 2017

Dynamics and mechanisms of pressure, heat release rate, and fuel spray coupling during intermittent thermoacoustic oscillations in a model aeronautical combustor at elevated pressure

Sina Kheirkhah; J. D. Maxim Cirtwill; Pankaj Saini; Krishna Venkatesan; Adam M. Steinberg


Combustion and Flame | 2014

Influence of edge velocity on flame front position and displacement speed in turbulent premixed combustion

Sina Kheirkhah; Ömer L. Gülder


55th AIAA Aerospace Sciences Meeting | 2017

Analysis of intermittent thermoacoustic oscillations in an aeronautical gas turbine combustor

Joseph D. Cirtwill; Sina Kheirkhah; Pankaj Saini; Krishna Venkatesan; Adam M. Steinberg


Combustion and Flame | 2016

On periodic behavior of weakly turbulent premixed flame corrugations

Sina Kheirkhah; Ömer L. Gülder; Guillaume Maurice; Fabien Halter; Iskender Gökalp


Journal of Fluids Engineering-transactions of The Asme | 2016

Wake Topology of a Cylinder Undergoing Vortex-Induced Vibrations With Elliptic Trajectories

Sina Kheirkhah; Serhiy Yarusevych; Sriram Narasimhan

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Christian Chauveau

Centre national de la recherche scientifique

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Fabien Thiesset

Centre national de la recherche scientifique

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Iskender Gökalp

Centre national de la recherche scientifique

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