Author:
Zhao Yuzhuo,Ma Dan,Ma Hongwei
Publisher
Springer Science and Business Media LLC
Subject
Information Systems,Computer Science (miscellaneous)
Reference30 articles.
1. Culick F E C and Yang V, Prediction of the stability of unsteady motions in solid-propellant rocket motors, American Institute of Aeronautics and Astronautics, 1992, 28: 719–779.
2. Richards G A, Straub D L, and Robey E H, Passive control of combustion dynamics in stationary gas turbines, Joumal of Propulsion and Power, 2003, 19: 795–810.
3. Gysling D L, Copeland G S, Mccormick D C, et al., Combustion system damping augmentation with Helmholtz resonator, Journal of Engineering for Gas Turbines and Power, 2000, 122(1): 269–274.
4. Eldredge J D and Dowling A P, The absorption of axial acoustic wave by a perforated liner with bias flow, Joumal of Fluid Mechanics, 2003, 485(1): 307–335.
5. Zhong Z, Time-domain characterization of acoustic damping of a perforated liner with bias flow, Journal of Acoustical America Society, 2012, 312(1): 271–281.
Cited by
10 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献