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Relevant bibliographies by topics / Rotating detonation engines

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Academic literature on the topic 'Rotating detonation engines'

Author: Grafiati

Published: 4 June 2021

Last updated: 25 January 2023

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Journal articles on the topic "Rotating detonation engines"

1

Wang, Yuhui, Wenyou Qiao, and JialingLe. "Combustion Characteristics in Rotating Detonation Engines." International Journal of Aerospace Engineering 2021 (March 13, 2021): 1–17. http://dx.doi.org/10.1155/2021/8839967.

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A lot of studies on rotating detonation engines have been carried out due to the higher thermal efficiency. However, the number, rotating directions, and intensities of rotating detonation waves are changeful when the flow rate, equivalence ratio, inflow conditions, and engine schemes vary. The present experimental results showed that the combustion mode of a rotating detonation engine was influenced by the combustor scheme. The annular detonation channel had an outer diameter of 100 mm and an inner diameter of 80 mm. Air and hydrogen were injected into the combustor from 60 cylindrical orific

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Xie, Qiaofeng, Zifei Ji, Haocheng Wen, Zhaoxin Ren, Piotr Wolanski, and Bing Wang. "Review on the Rotating Detonation Engine and It’s Typical Problems." Transactions on Aerospace Research 2020, no. 4 (2020): 107–63. http://dx.doi.org/10.2478/tar-2020-0024.

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Abstract Detonation is a promising combustion mode to improve engine performance, increase combustion efficiency, reduce emissions, and enhance thermal cycle efficiency. Over the last decade, significant progress has been made towards the applications of detonation mode in engines, such as standing detonation engine (SDE), Pulse detonation engine (PDE) and rotating detonation engine (RDE), and the understanding of the fundamental chemistry and physics processes in detonation engines via experimental and numerical studies. This article is to provide a comprehensive overview of the progress in t

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3

Ji, Zifei, Ruize Duan, Renshuai Zhang, Huiqiang Zhang, and Bing Wang. "Comprehensive Performance Analysis for the Rotating Detonation-Based Turboshaft Engine." International Journal of Aerospace Engineering 2020 (July 2, 2020): 1–11. http://dx.doi.org/10.1155/2020/9587813.

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The potential advantages of rotating detonation combustion are gradually approved, and it is becoming a stable and controllable energy conversion way adopted to the propulsion devices or ground-engines. This study focuses on the rotating detonation-based turboshaft engine, and the architecture is presented for this form of engine with compatibility between the turbomachinery and rotating detonation combustor being realized. The parametric performance simulation model for the rotating detonation-based turboshaft engine are developed. Further, the potential performance benefits as well as their

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Sosa, Jonathan, Kareem A. Ahmed, Robert Fievisohn, John Hoke, Timothy Ombrello, and Frederick Schauer. "Supersonic driven detonation dynamics for rotating detonation engines." International Journal of Hydrogen Energy 44, no. 14 (2019): 7596–606. http://dx.doi.org/10.1016/j.ijhydene.2019.02.019.

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Wang, Yu Hui, and Jian Ping Wang. "Rotating Detonation Instabilities in Hydrogen-Oxygen Mixture." Applied Mechanics and Materials 709 (December 2014): 56–62. http://dx.doi.org/10.4028/www.scientific.net/amm.709.56.

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Rotating detonation engines are studied more and more widely because of high thermodynamic efficiency and high specific impulse. Rotating detonation of hydrogen and oxygen was achieved in this study. Rotating detonation waves were observed by high speed cameras and detonation pressure traces were recorded by PCB pressure sensors. The velocity of rotating detonation waves is fluctuating during the run. Low frequency detonation instabilities, intermediate frequency detonation instabilities and high frequency detonation instabilities were discovered. They are relevant to unsteady heat release, ac

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Zhou, Jianping, Feilong Song, Shida Xu, Xingkui Yang, and Yongjun Zheng. "Investigation of Rotating Detonation Fueled by Liquid Kerosene." Energies 15, no. 12 (2022): 4483. http://dx.doi.org/10.3390/en15124483.

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The performance of rotating detonation engines (RDEs) is theoretically better than that of traditional aero engines because of self-pressurization. A type of swirl injection scheme is introduced in this paper for two-phase detonation. On the one hand, experiments are performed on continuous rotating detonation of ternary “kerosene, hydrogen and oxygen-enriched air” mixture in an annular combustor. It is found that increasing the mass fraction of hydrogen can boost the wave speed and the stability of detonation waves’ propagation. One the other hand, characteristics of kerosene–hot air RDE is i

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Zhou, Rui, Dan Wu, and Jianping Wang. "Progress of continuously rotating detonation engines." Chinese Journal of Aeronautics 29, no. 1 (2016): 15–29. http://dx.doi.org/10.1016/j.cja.2015.12.006.

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Wang, Yuhui, and Jianping Wang. "Coexistence of detonation with deflagration in rotating detonation engines." International Journal of Hydrogen Energy 41, no. 32 (2016): 14302–9. http://dx.doi.org/10.1016/j.ijhydene.2016.06.026.

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Batista, Armani, Mathias C. Ross, Christopher Lietz, and William A. Hargus. "Descending Modal Transition Dynamics in a Large Eddy Simulation of a Rotating Detonation Rocket Engine." Energies 14, no. 12 (2021): 3387. http://dx.doi.org/10.3390/en14123387.

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Rotating detonation rocket engines (RDREs) exhibit various unsteady phenomena, including modal transitions, that significantly affect their operation, performance and stability. The dynamics of the detonation waves are studied during a descending modal transition (DMT) where four co-rotating detonations waves decrease to three in a gaseous methane-oxygen RDRE. Detonation wave tracking is applied to capture, visualize and analyze unsteady, 3D detonation wave dynamics data within the combustion chamber of the RDRE. The mechanism of a descending modal transition is the failure of a detonation wav

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Frolov, Sergey M., Igor O. Shamshin, Viktor S. Aksenov, Vladislav S. Ivanov, and Pavel A. Vlasov. "Ion Sensors for Pulsed and Continuous Detonation Combustors." Chemosensors 11, no. 1 (2023): 33. http://dx.doi.org/10.3390/chemosensors11010033.

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Presented in the article are the design and operation principles of ion sensors intended for detecting the propagating reaction fronts, the deflagration/detonation mode, apparent subsonic/supersonic propagation velocity of the reaction front, and duration of heat release by measuring the ion current in the reactive medium. The electrical circuits for ion sensors without and with intermediate amplifiers, with short response time and high sensitivity, as well as with the very wide dynamic range of operation in the reactive media with highly variable temperature and pressure, are provided and dis

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Dissertations / Theses on the topic "Rotating detonation engines"

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Anand, Vijay G. "Rotating Detonation Combustor Mechanics." University of Cincinnati / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1530798871271548.

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Lim, Wei Han Eugene. "Gasdynamic inlet isolation in rotating detonation engine." Thesis, Monterey, California. Naval Postgraduate School, 2010. http://hdl.handle.net/10945/5068.

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Includes supplementary material<br>Approved for public release; distribution is unlimited<br>The Rotating Detonation Engine (RDE) concept represents the next-generation of detonation-based engines as it provides higher performance and near constant thrust with a simpler overall design. Since RDE systems are in the early stage of development, the physics of engine design is yet to be fully understood and developed. A critical concern of these systems is the practical isolation of the reactant injection manifold and supply system from the combustor pressure oscillations. For this study, the

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Driscoll, Robert B. "Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System." University of Cincinnati / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1459155478.

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North, Gary S. "Metal Coupon Testing in an Axial Rotating Detonation Engine for Wear Characterization." Wright State University / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=wright1588770787704665.

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Subramanian, Sathyanarayanan. "Novel Approach for Computational Modeling of a Non-Premixed Rotating Detonation Engine." Thesis, Virginia Tech, 2019. http://hdl.handle.net/10919/101777.

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Detonation cycles are identified as an efficient alternative to the Brayton cycles used in power and propulsion applications. Rotating Detonation Engine (RDE) operating on a detonation cycle works by compressing the working fluid across a detonation wave, thereby reducing the number of compressor stages required in the thermodynamic cycle. Numerical analyses of RDEs are flexible in understanding the flow field within the RDE, however, three-dimensional analyses are expensive due to the differences in time-scale required to resolve the combustion process and flow-field. The alternate two-dimens

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Suchocki, James Alexander. "Operational Space and Characterization of a Rotating Detonation Engine Using Hydrogen and Air." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1330266587.

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Wilhite, Jarred M. "Investigation of Various Novel Air-Breathing Propulsion Systems." University of Cincinnati / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=ucin147981623341895.

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Hansmetzger, Sylvain. "Etude des modes de rotation continue d'une détonation dans une chambre annulaire de section constante ou croissante." Thesis, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique, 2018. http://www.theses.fr/2018ESMA0002/document.

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Notre étude vise à améliorer la compréhension des modes de rotation continue d’une détonation. Elle porte sur leur caractérisation dans une chambre annulaire de section,normale à son axe de révolution, constante ou linéairement croissante. Le principe de fonctionnement repose sur l’injection continue de gaz frais devant le front de détonation pour renouveler la couche réactive et entretenir sa propagation. Ce travail trouve son application dans le développement de systèmes propulsifs utilisant la détonation rotative comme mode de combustion (Rotating Detonation Engine, RDE). Nous avons conçu e

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(11014821), Ian V. Walters. "Operability and Performance of Rotating Detonation Engines." Thesis, 2021.

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<div>Rotating Detonation Engines (RDEs) provide a promising avenue for reducing greenhouse gas emissions from combustion-based propulsion and power systems by improving their thermodynamic efficiency through the application of pressure-gain combustion. However, the thermodynamic and systems-level advantages remain unrealized due to the challenge of harnessing the tightly coupled physics and nonlinear detonation dynamics inherent to RDEs, particularly for the less-detonable reactants characteristic of applications. Therefore, a RDE was developed to operate with natural gas and air as the primar

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(6927776), Alexis Joy Harroun. "Investigation of Nozzle Performance for Rotating Detonation Rocket Engines." Thesis, 2019.

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Progress in conventional rocket engine technologies, based on constant pressure combustion, has plateaued in the past few decades. Rotating detonation engines (RDEs) are of particular interest to the rocket propulsion community as pressure gain combustion may provide improvements to specific impulse relevant to booster applications. Despite recent significant investment in RDE technologies, little research has been conducted to date into the effect of nozzle design on rocket application RDEs. Proper nozzle design is critical to capturing the thrust potential of the transient pressure ratios pr

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Books on the topic "Rotating detonation engines"

1

Wang, Cheng, Jiun-Ming Li, Chiang Juay Teo, Boo Cheong Khoo, and Jian-Ping Wang. Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines. Springer, 2018.

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Wang, Cheng, Jiun-Ming Li, Chiang Juay Teo, Boo Cheong Khoo, and Jian-Ping Wang. Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines. Springer, 2017.

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Book chapters on the topic "Rotating detonation engines"

1

Fotia, Matthew L., John Hoke, and Frederick Schauer. "Performance of Rotating Detonation Engines for Air Breathing Applications." In Shock Wave and High Pressure Phenomena. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-68906-7_1.

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Kailasanath, K. "Injector Dynamics and Pressure Gain in Rotating Detonation Engines." In Green Energy and Technology. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-2648-7_1.

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Liu, Xiang-Yang, Yan-Liang Chen, Song-Bai Yao, and Jian-Ping Wang. "Numerical Study of Reverse-Rotating Wave in the Hollow Rotating Detonation Engines." In Lecture Notes in Electrical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_134.

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Chang, Po-Hsiung, Jiun-Ming Li, Boo Cheong Khoo, Lei Li, Jie Ming Teh, and Chiang Juay Teo. "Design and Measurement of Injection Gas Concertation in Rotating Detonation Engines via Diode Laser Sensors." In 31st International Symposium on Shock Waves 2. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91017-8_17.

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Ramanujachari, V., Rahul Dutta Roy, and P. Amrutha Preethi. "Design and Analysis of Rotating Detonation Wave Engine." In Proceedings of the National Aerospace Propulsion Conference. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2378-4_24.

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Nejaamtheen, Mohammed Niyasdeen, Jung-Min Kim, and Jeong-Yeol Choi. "Review on the Research Progresses in Rotating Detonation Engine." In Shock Wave and High Pressure Phenomena. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-68906-7_6.

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Tsuboi, Nobuyuki, Makoto Asahara, Takayuki Kojima, and A. Koichi Hayashi. "Numerical Simulation on Rotating Detonation Engine: Effects of Higher-Order Scheme." In Shock Wave and High Pressure Phenomena. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-68906-7_5.

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Nishimura, J., K. Ishihara, K. Goto, et al. "Experimental Research on a Long-Duration Operation of a Rotating Detonation Engine." In 31st International Symposium on Shock Waves 2. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91017-8_15.

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Ramanujachari, V., Rahul Dutta Roy, and P. Amrutha Preethi. "Design and Performance Evaluation of Plug Nozzle for Rotating Detonation Wave Engine." In Proceedings of the National Aerospace Propulsion Conference. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-2378-4_25.

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Wang, Jian-Ping, and Ye-Tao Shao. "Rotating Detonation Engine Injection Velocity Limit and Nozzle Effects on Its Propulsion Performance." In Computational Fluid Dynamics 2010. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-17884-9_100.

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Conference papers on the topic "Rotating detonation engines"

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Appalla, Lakshmi Sumedha, Raja Joseph, and V. Ramanuja Chari. "Investigations on rotating detonation engines." In 3RD INTERNATIONAL CONFERENCE ON FRONTIERS IN AUTOMOBILE AND MECHANICAL ENGINEERING (FAME 2020). AIP Publishing, 2020. http://dx.doi.org/10.1063/5.0035437.

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IVANOV, V. S., S. S. SERGEEV, S. M. FROLOV, YU M. MIRONOV, A. E. NOVIKOV, and I. I. SCHULZ. "PRESSURE MEASUREMENTS IN ROTATING DETONATION ENGINES." In 12TH INTERNATIONAL COLLOQUIUM ON PULSED AND CONTINUOUS DETONATIONS. TORUS PRESS, 2020. http://dx.doi.org/10.30826/icpcd12a28.

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The use of Rotating Detonation Engines (RDEs) is a promising way to efficiently convert the chemical energy of fuel into the mechanical energy for propulsion. The values of local pressure in the RDEs are the most important indicators of the operation process efficiency. Pressure sensors in RDEs are exposed to high temperatures ( 3000 K) and pressures (10 MPa), as well as mechanical vibrations. Therefore, the duration of test fires of RDEs with pressure sensors mounted directly in the RDE walls is usually very short (from tenths of a second to several seconds) to avoid sensors£ destruction.

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R., SHAN, LI J.M., TEO C.J., and KHOO B.C. "NUMERICAL INVESTIGATIONOF ETHYLENE-FUELED ROTATING DETONATION ENGINES." In 10th International Workshop on Detonation for Propulsion (IWDP). TORUS PRESS, 2019. http://dx.doi.org/10.30826/iwdp201909.

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Schwer, Douglas, and Kailas Kailasanath. "Numerical Investigation of Rotating Detonation Engines." In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-6880.

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Martinez, Ariana G., and Stephen D. Heister. "Wave Structure of Heterogeneous Detonations in Rotating Detonation Rocket Engines." In AIAA SCITECH 2022 Forum. American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-0091.

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Whitman, Charles R., Chibuikem U. Ajaero, Sean Connolly-Boutin, Xavier L'espérance, Charles Kiyanda, and Andrew J. Higgins. "Computational Simulation of Multiheaded Detonation Dynamics in Rotating Detonation Engines." In AIAA Propulsion and Energy 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-3877.

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Lietz, Christopher, Nathan L. Mundis, Stephen A. Schumaker, and Venke Sankaran. "Numerical Investigation of Rotating Detonation Rocket Engines." In 2018 AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0882.

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Schwer, Douglas, and Kailas Kailasanath. "Modeling Exhaust Effects in Rotating Detonation Engines." In 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-3943.

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Bennewitz, John W., Jason R. Burr, and Christopher F. Lietz. "Characteristic Timescales for Rotating Detonation Rocket Engines." In AIAA Propulsion and Energy 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-3671.

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Schneider, Robson Eduardo dos Anjos, Cesar Celis, and Andrés Armando Mendiburu Zevallos. "Thermodynamic Modelling of Rotating Detonation Engines Cycles." In 19th Brazilian Congress of Thermal Sciences and Engineering. ABCM, 2022. http://dx.doi.org/10.26678/abcm.encit2022.cit22-0104.

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Reports on the topic "Rotating detonation engines"

1

Gamba, Mirko, and Venkat Raman. A Joint Experimental/Computational Study of Non-Idealities in Practical Rotating Detonation Engines. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1601159.

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Weber, Justin. Rotating Detonation Engine Introduction. Office of Scientific and Technical Information (OSTI), 2021. http://dx.doi.org/10.2172/1871020.

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