Adaptive operating mode switching process in rotating detonation engines

被引:10
作者
Yao, Songbai [1 ,3 ]
Tang, Xinmeng [2 ]
Zhang, Wenwu [1 ,3 ]
机构
[1] Chinese Acad Sci, Ningbo Inst Mat Technol & Engn, Zhejiang Key Lab Aero Engine Extreme Mfg Technol, Ningbo 315201, Peoples R China
[2] Innovat Ctr Tsinghna Univ, Shanghai 200062, Peoples R China
[3] Univ Chinese Acad Sci, Beijing 100049, Peoples R China
关键词
Rotating detonation; Operating mode; Stability; Numerical simulation; Quasi-steady analysis; PERFORMANCE ANALYSIS; MIXTURE; STABILITY; WAVE;
D O I
10.1016/j.actaastro.2023.01.019
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this study, the adaptive mode switching process of rotating detonation waves (RDWs) in response to the change of inlet conditions is numerically explored and analytically explained. Once a quasi-steady rotating detonation flow field is obtained, the inlet total pressure of the reservoir is decreased and maintained at different levels for a certain period of time in order to observe the feedback on the RDWs. It shows that instead of being quenched immediately, the RDWs can adapt to the change of inlet conditions by a mode switching adjustment; it decreases the number of detonation waves and begins to run in a new operating mode, a process that is found to occur swiftly and is corroborated by experimental observations; moreover, an analytical analysis indicates that for a stable RDW flow field, the characteristic parameters such as the number and height of detonation waves are related to the combustor geometry and inlet conditions, which determine whether the RDWs are required to switch into a new operating mode as a means to ensure stability. Additionally, the results indicate that the rotating detonation engine (RDE) can work in different operating modes at the same mass flow rate, or conversely, the RDE can remain in the same operating mode even if the mass flow rate varies.
引用
收藏
页码:239 / 246
页数:8
相关论文
共 58 条
[1]   Black-Box Modeling of Rotating Detonation Combustors and Their Injector Plena Coupling [J].
Anand, Vijay ;
St George, Andrew ;
Jodele, Justas ;
Knight, Ethan ;
Gutmark, Ephraim .
AIAA JOURNAL, 2020, 58 (12) :5095-5106
[2]   Rotating detonation combustors and their similarities to rocket instabilities [J].
Anand, Vijay ;
Gutmark, Ephraim .
PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2019, 73 :182-234
[3]   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
[4]  
[Anonymous], 1960, Sov. J. Appl. Mech. Tech. Phys., V3, P164
[5]   Performance analysis of a rotating detonation combustor based on stagnation pressure measurements [J].
Bach, Eric ;
Stathopoulos, Panagiotis ;
Paschereit, Christian Oliver ;
Bohon, Myles D. .
COMBUSTION AND FLAME, 2020, 217 :21-36
[6]   Monotonicity preserving weighted essentially non-oscillatory schemes with increasingly high order of accuracy [J].
Balsara, DS ;
Shu, CW .
JOURNAL OF COMPUTATIONAL PHYSICS, 2000, 160 (02) :405-452
[7]   3D numerical modeling of a cylindrical RDE with an inner body extending out of the nozzle [J].
Betelin, V. B. ;
Nikitin, V. F. ;
Mikhalchenko, E., V .
ACTA ASTRONAUTICA, 2020, 176 :628-646
[8]   Continuous spin detonations [J].
Bykovskii, Fedor A. ;
Zhdan, Sergey A. ;
Vedernikov, Evgenii F. .
JOURNAL OF PROPULSION AND POWER, 2006, 22 (06) :1204-1216
[9]  
Canteins G., 2006, Etude de la detonation continue rotative-Application Aa la propulsion
[10]  
Ciccarelli G., 1997, Detonation Cell Size Measurements in High-Temperature Hydrogen-Air-Steam Mixtures at the BNL High-Temperature Combustion Facility