Limit Cycle Oscillating Detonation Wave Behavior Analysis Within a Rotating Detonation Engine

被引:0
作者
May, Kristyn B. Johnson [1 ]
Weber, Justin [1 ]
Ferguson, Don [1 ]
Nix, Andrew [2 ]
Sidwell, Todd G. [3 ]
机构
[1] Natl Energy Technol Lab, Thermal Sci, Morgantown, WV 26505 USA
[2] West Virginia Univ, Mech & Aerosp Engn, Morgantown, WV 26505 USA
[3] Natl Energy Technol Lab, Mech & Aerosp Engn, Morgantown, WV 26505 USA
关键词
Combustion Instability; Rotating Detonation Combustor; Optical Properties; Gas Turbine Engines; Data Acquisition; Detonation Waves; Rotating Detonation Engine; Oscillatory Dynamics; Pressure Gain Combustion; CHEMILUMINESCENCE;
D O I
10.2514/1.B39271
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Limit cycle oscillation (LCO) detonation wave behaviors are presented and analyzed for test times exceeding 20 s in a water-cooled rotating detonation engine (RDE). LCO detonation waves exhibit cyclic acceleration and deceleration, resulting in oscillating wave spacing at unique process conditions. In previous RDE studies, similar behaviors have been studied as microsecond-scale instabilities leading to ascending or descending modal transitions. In the current work, however, LCO waves are considered a persistent wave mode, occupying unique portions of the operational envelope adjacent to those of their equally spaced counterparts. These occurrences of LCO waves are repeatable, enduring behaviors. A method to generate shifted contour surfaces specifically intended to extract and analyze wave spacing variation through time, termed limit cycle oscillation visualization (LCOV) surfaces, is presented. LCOV surfaces transform data into the reference frame of a primary traveling wave and are used to analyze quasi-steady, short-timescale, and transitional LCO modes. Results are leveraged to understand the relationship between fill height, wave strength, local wave acceleration, and subsequent LCO wave spacing for individual wave sets. Quasi-steady LCO waves display wave spacing oscillations between equal spacing values associated with +/- 1 wave across runs exceeding 18 s.
引用
收藏
页码:701 / 716
页数:16
相关论文
共 24 条
[1]   Impact of gas turbine flexibility improvements on combined cycle gas turbine performance [J].
Abudu, Kamal ;
Igie, Uyioghosa ;
Roumeliotis, Ioannis ;
Hamilton, Richard .
APPLIED THERMAL ENGINEERING, 2021, 189
[2]   Characterization of instabilities in a Rotating Detonation Combustor [J].
Anand, Vijay ;
St George, Andrew ;
Driscoll, Robert ;
Gutmark, Ephraim .
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2015, 40 (46) :16649-16659
[3]   Descending Modal Transition Dynamics in a Large Eddy Simulation of a Rotating Detonation Rocket Engine [J].
Batista, Armani ;
Ross, Mathias C. ;
Lietz, Christopher ;
Hargus, William A., Jr. .
ENERGIES, 2021, 14 (12)
[4]   Automated image processing method to quantify rotating detonation wave behavior [J].
Bennewitz, J. W. ;
Bigler, B. R. ;
Schumaker, S. A. ;
Hargus, W. A., Jr. .
REVIEW OF SCIENTIFIC INSTRUMENTS, 2019, 90 (06)
[5]   MODAL TRANSITIONS IN ROTATING DETONATION ROCKET ENGINES [J].
Bennewitz, John W. ;
Bigler, Blaine R. ;
Pilgram, Jessica J. ;
Hargus, William A., Jr. .
INTERNATIONAL JOURNAL OF ENERGETIC MATERIALS AND CHEMICAL PROPULSION, 2019, 18 (02) :91-109
[6]   Counter-rotating wave mode transition dynamics in an RDC [J].
Bluemner, R. ;
Bohon, M. D. ;
Paschereit, C. O. ;
Gutmark, E. J. .
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2019, 44 (14) :7628-7641
[7]  
Boening J.A., 2016, AIAA Paper 2016-4966, DOI DOI 10.2514/6.2016-4966
[8]  
Brophy C M., 2019, AIAA Propulsion and Energy 2019 Forum, DOI DOI 10.2514/6.2019-4212
[9]  
Feleo A, 2019, AIAA SCITECH 2019 FORUM
[10]  
FERGUSON D, 2020, AIAA SCITECH 2020 FO