Finding the Cause of a Fatal Problem in Rocket Engine Combustors
Via advanced analyses, scientists shed light on the mechanism of a deadly problem plaguing combustion chambers in rocket engines
A vital piece of gas engines, combustors―the chambers in which the combustion powering the engine occurs―have the problem of breaking down due to fatal high-frequency oscillations during the combustion process. Now, through advanced time-series analyses based on complex systems, researchers from Tokyo University of Science and Japan Aerospace Exploration Agency have found what causes them, opening up novel paths to solving the problem.
Rocket engines contain confined combustion systems, which are, essentially, combustion chambers. In these chambers, nonlinear interactions among turbulent fuel and oxidizer flows, sound waves, and heat produced from chemical reactions, cause an unstable phenomenon called 'combustion oscillations.' The force of these oscillations on the body of the combustion chamber―the mechanical stress on the chamber― is high enough to threaten catastrophic failure of the engine. What causes these oscillations? The answer remains to be found.
Now, in a breakthrough, published in Physics of Fluids, a team including Prof. Hiroshi Gotoda, Ms. Satomi Shima, and Mr. Kosuke Nakamura from Tokyo University of Science (TUS), in collaboration with Dr. Shingo Matsuyama and Dr. Yuya Ohmichi from the Japan Aerospace Exploration Agency (JAXA), have used advanced time-series analyses based on complex systems to find out.
Explaining their work, Prof. Gotoda says, "Our main purpose was to reveal the physical mechanism behind the formation and sustenance of high-frequency combustion oscillations in a cylindrical combustor using sophisticated analytical methods inspired by symbolic dynamics and complex networks." These findings have also been covered by the American Society of Physics in their news section, and by the Institute of Physics on their news platform Physics World.
The combustor the scientists picked to simulate is one of model rocket engines. They were able to pinpoint the moment of transition from the stable combustion state to combustion oscillations and visualize it. They found that significant periodic flow velocity fluctuations in fuel injector affect the ignition process, resulting in changes to the heat release rate. The heat release rate fluctuations synchronize with the pressure fluctuations inside the combustor, and the whole cycle continues in a series of feedback loops that sustain combustion oscillations.
Additionally, by considering a spatial network of pressure and heat release rate fluctuations, the researchers found that clusters of acoustic power sources periodically form and collapse in the shear layer of the combustor near the injection pipe's rim, further helping drive the combustion oscillations.
These findings provide reasonable answers for why combustion oscillations occur, albeit specific to liquid rocket engines. Prof. Gotoda explains, "Combustion oscillations can cause fatal damage to combustors in rocket engines, aero engines, and gas turbines for power generation. Therefore, understanding the formation mechanism of combustion oscillations is an important research subject. Our results will greatly contribute to our understanding of the mechanism of combustion oscillations generated in liquid rocket engines."
Indeed, these findings are significant and can be expected to open doors to novel routes of exploration to prevent combustion oscillations in critical engines.
Representation of instantaneous flow velocity field during combustion oscillations in the combustion chamber of a model rocket engine
This figure shows that large-scale vortex rings are produced from the injector rim during combustion oscillations.
Photo courtesy: Satomi Shima, Kosuke Nakamura, Hiroshi Gotoda, Yuya Ohmichi, and Shingo Matsuyama
|Title of original paper||:||Formation mechanism of high-frequency combustion oscillations in a model rocket engine combustor|
|Journal||:||Physics of Fluids|
Tokyo University of Science (TUS) is a well-known and respected university, and the largest science-specialized private research university in Japan, with four campuses in central Tokyo and its suburbs and in Hokkaido. Established in 1881, the university has continually contributed to Japan's development in science through inculcating the love for science in researchers, technicians, and educators.
With a mission of "Creating science and technology for the harmonious development of nature, human beings, and society", TUS has undertaken a wide range of research from basic to applied science. TUS has embraced a multidisciplinary approach to research and undertaken intensive study in some of today's most vital fields. TUS is a meritocracy where the best in science is recognized and nurtured. It is the only private university in Japan that has produced a Nobel Prize winner and the only private university in Asia to produce Nobel Prize winners within the natural sciences field.
About Professor Hiroshi Gotoda from Tokyo University of Science
Dr. Hiroshi Gotoda is a Professor of the Department of Mechanical Engineering at Tokyo University of Science, Japan. He obtained his Ph.D. from Keio University, Japan. He currently heads the Chemically Reactive and Thermal Engineering Laboratory at TUS where his focus of research is the study on nonlinear dynamics of thermal fluids using dynamical systems theory.