This work is motivated by the thermoacoustic instability challenges associated with ultra-low emissions gas turbine (GT) combustors. It demonstrates the first use of high-speed dual-plane orthogonally-polarized stereoscopic-particle image velocimetry (PIV) and synchronized OH planar laser-induced fluorescence in a premixed swirling flame. We use this technique to explore the effects of combustion and longitudinal acoustic forcing on the time- and phase-averaged flow field—particularly focusing on the behavior of the Reynolds stress in the presence of harmonic forcing. We observe significant differences between ensemble-averaged and time-averaged Reynolds stress. This implies that the large-scale motions are nonergodic, due to coherent oscillations in Reynolds stress associated with the convection of periodic vortical structures. This result has important implications on hydrodynamic stability models and reduced-order computational fluid dynamics simulations, which do show the importance of turbulent transport on the problem, but do not capture these coherent oscillations in their models.
Skip Nav Destination
Article navigation
January 2019
Research-Article
Measurements of Periodic Reynolds Stress Oscillations in a Forced Turbulent Premixed Swirling Flame
Christopher Douglas,
Christopher Douglas
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
e-mail: cmdouglas@gatech.edu
Georgia Institute of Technology,
Atlanta, GA 30332
e-mail: cmdouglas@gatech.edu
Search for other works by this author on:
Jamie Lim,
Jamie Lim
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Search for other works by this author on:
Travis Smith,
Travis Smith
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Search for other works by this author on:
Benjamin Emerson,
Benjamin Emerson
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Search for other works by this author on:
Timothy Lieuwen,
Timothy Lieuwen
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Search for other works by this author on:
Naibo Jiang,
Naibo Jiang
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Search for other works by this author on:
Christopher Fugger,
Christopher Fugger
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Search for other works by this author on:
Tongxun Yi,
Tongxun Yi
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Search for other works by this author on:
Josef Felver,
Josef Felver
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Search for other works by this author on:
James Gord
James Gord
Air Force Research Laboratory,
Aerospace Systems Directorate,
Wright-Patterson AFB, OH 45433
e-mail: james.gord@us.af.mil
Aerospace Systems Directorate,
Wright-Patterson AFB, OH 45433
e-mail: james.gord@us.af.mil
Search for other works by this author on:
Christopher Douglas
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
e-mail: cmdouglas@gatech.edu
Georgia Institute of Technology,
Atlanta, GA 30332
e-mail: cmdouglas@gatech.edu
Jamie Lim
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Travis Smith
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Benjamin Emerson
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Timothy Lieuwen
Ben T. Zinn Combustion Lab,
Georgia Institute of Technology,
Atlanta, GA 30332
Georgia Institute of Technology,
Atlanta, GA 30332
Naibo Jiang
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Christopher Fugger
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Tongxun Yi
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Josef Felver
Spectral Energies, LLC,
Dayton, OH 45430
Dayton, OH 45430
Sukesh Roy
James Gord
Air Force Research Laboratory,
Aerospace Systems Directorate,
Wright-Patterson AFB, OH 45433
e-mail: james.gord@us.af.mil
Aerospace Systems Directorate,
Wright-Patterson AFB, OH 45433
e-mail: james.gord@us.af.mil
Manuscript received June 22, 2018; final manuscript received June 25, 2018; published online August 31, 2018. Editor: Jerzy T. Sawicki.
J. Eng. Gas Turbines Power. Jan 2019, 141(1): 011001 (9 pages)
Published Online: August 31, 2018
Article history
Received:
June 22, 2018
Revised:
June 25, 2018
Citation
Douglas, C., Lim, J., Smith, T., Emerson, B., Lieuwen, T., Jiang, N., Fugger, C., Yi, T., Felver, J., Roy, S., and Gord, J. (August 31, 2018). "Measurements of Periodic Reynolds Stress Oscillations in a Forced Turbulent Premixed Swirling Flame." ASME. J. Eng. Gas Turbines Power. January 2019; 141(1): 011001. https://doi.org/10.1115/1.4040686
Download citation file:
Get Email Alerts
Cited By
Shape Optimization of an Industrial Aeroengine Combustor to reduce Thermoacoustic Instability
J. Eng. Gas Turbines Power
Dynamic Response of A Pivot-Mounted Squeeze Film Damper: Measurements and Predictions
J. Eng. Gas Turbines Power
Review of The Impact Of Hydrogen-Containing Fuels On Gas Turbine Hot-Section Materials
J. Eng. Gas Turbines Power
Effects of Lattice Orientation Angle On Tpms-Based Transpiration Cooling
J. Eng. Gas Turbines Power
Related Articles
Combustion Instabilities and Control of a Multiswirl Atmospheric Combustor
J. Eng. Gas Turbines Power (January,2007)
A Large-Eddy Simulation–Linear-Eddy Model Study of Preferential Diffusion Processes in a Partially Premixed Swirling Combustor With Synthesis Gases
J. Eng. Gas Turbines Power (March,2017)
Damkohler Number Analysis in Lean Blow-Out of Toroidal Jet Stirred Reactor
J. Eng. Gas Turbines Power (October,2018)
Stabilization Mechanisms of Swirling Premixed Flames With an Axial-Plus-Tangential Swirler
J. Eng. Gas Turbines Power (August,2018)
Related Chapters
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Combustion Under Harmonically Oscillating Pressure
Theory of Solid-Propellant Nonsteady Combustion
The Identification of the Flame Combustion Stability by Combining Principal Component Analysis and BP Neural Network Techniques
International Conference on Mechanical Engineering and Technology (ICMET-London 2011)