Study on Hysteresis of Combustion Oscillation in Continuously Variable Resonance Combustor using Deep Neural Network
Author:
Affiliation:
1. College of Science and Technology, Nihon University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/19/4/19_19.570/_pdf
Reference11 articles.
1. 1) Lord Rayleigh, The Explanation of Certain Acoustical Phenomena, Nature, 18 (1878), pp. 319-321.
2. 2) Tanabe, M., Saito, M., Hallum, W. Z., Meier, E. J., Fuller, T. L., and Anderson, W. E.: Self-Excited Non-Linear Acoustic Wave in a Single-Element Model Rocket Combustor and Its Influence on Flame, Trans. JSASS Aerospace Technology Japan, 14, ists30 (2016), pp. Pa_1–Pa_6.
3. 3) Yu, Y., Sisco, J. C., Rosen, S., Madhav, A., and Anderson, W. E.: Spontaneous Longitudinal Combustion Instability in a Continuously-Variable Resonance Combustor, J. Propulsion and Power, 28 (2012), pp. 876–887.
4. 4) Harvazinski, M. E., Huang, C., Sankaran, V., Feldman, T. W., Anderson, W. E., Merkle, C. L., and Talley, D. G.: Coupling between Hydrodynamics, Acoustics, and Heat Release in a Selfexcited Unstable Combustor, Physics of Fluids, 27 (2015), pp. 045102_1-045102_27.
5. 5) Hardi, J., Hallum, W. Z., Huang, C., and Anderson, W. E.: Development of Validation Approaches for Numerical Simulation of Combustion Instability using Flame Imaging, AIAA Paper 2014-3775, 2014.
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1. Study on Nonlinear Dynamics Using the State Space of Combustion Oscillation in a Rocket Combustor;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023
2. Analysis of spatial-temporal dynamics of cool flame oscillation phenomenon occurred around a fuel droplet array by using variational auto-encoder;Proceedings of the Combustion Institute;2022-11
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