Thematische Bibliographien / Rotating Detonations

Inhaltsverzeichnis

  1. Zeitschriftenartikel
  2. Dissertationen
  3. Bücher
  4. Buchteile
  5. Konferenzberichte
  6. Berichte der Organisationen

Auswahl der wissenschaftlichen Literatur zum Thema „Rotating Detonations“

Autor: Grafiati
Veröffentlicht am 4. Juni 2021
Zuletzt aktualisiert am 6. Februar 2022

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Zeitschriftenartikel zum Thema "Rotating Detonations"

1

Zhang, Hailong, Weidong Liu, Lin Zhang, Shijie Liu, and Luxin Jiang. "Effects of Chamber Width on H2/Air Rotating Detonations." International Journal of Aerospace Engineering 2020 (October 20, 2020): 1–14. http://dx.doi.org/10.1155/2020/8819667.

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To get the effects of chamber width on the H2/Air rotating detonations, several models with different widths have been investigated. By using a one-step chemical reaction model, one wave is induced in all models. The chamber width has a significant effect on the flow field. When the chamber width is small, the variation of the flow field with the radius is not obvious. But when the width increases, the curvature of the detonation wave reflecting between the inner and outer walls at the head would become enlarged. The height of the detonation wave both on the inner wall and the outer wall has b
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Fink, M., M. Kromer, W. Hillebrandt, et al. "Thermonuclear explosions of rapidly differentially rotating white dwarfs: Candidates for superluminous Type Ia supernovae?" Astronomy & Astrophysics 618 (October 2018): A124. http://dx.doi.org/10.1051/0004-6361/201833475.

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The observed sub-class of “superluminous” Type Ia supernovae lacks a convincing theoretical explanation. If the emission of such objects were powered exclusively by radioactive decay of 56Ni formed in the explosion, a progenitor mass close to or even above the Chandrasekhar limit for a non-rotating white dwarf star would be required. Masses significantly exceeding this limit can be supported by differential rotation. We, therefore, explore explosions and predict observables for various scenarios resulting from differentially rotating carbon–oxygen white dwarfs close to their respective limit o
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Hishida, Manabu, Toshi Fujiwara, and Piotr Wolanski. "Fundamentals of rotating detonations." Shock Waves 19, no. 1 (2009): 1–10. http://dx.doi.org/10.1007/s00193-008-0178-2.

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4

Anand, Vijay, and Ephraim Gutmark. "Rotating Detonations and Spinning Detonations: Similarities and Differences." AIAA Journal 56, no. 5 (2018): 1717–22. http://dx.doi.org/10.2514/1.j056892.

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5

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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García-Senz, D., R. M. Cabezón, and I. Domínguez. "Surface and Core Detonations in Rotating White Dwarfs." Astrophysical Journal 862, no. 1 (2018): 27. http://dx.doi.org/10.3847/1538-4357/aacb7d.

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7

St. George, A., R. Driscoll, V. Anand, and E. Gutmark. "On the existence and multiplicity of rotating detonations." Proceedings of the Combustion Institute 36, no. 2 (2017): 2691–98. http://dx.doi.org/10.1016/j.proci.2016.06.132.

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8

Jodele, Justas, Vijay Anand, Alexander Zahn, Nathan Chiles, and Ephraim Gutmark. "Quantification of Rotating Detonations Using OH* Chemiluminescence at Varied Widths." AIAA Journal 59, no. 7 (2021): 2457–66. http://dx.doi.org/10.2514/1.j059737.

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9

Teng, Honghui, Lin Zhou, Pengfei Yang, and Zonglin Jiang. "Numerical investigation of wavelet features in rotating detonations with a two-step induction-reaction model." International Journal of Hydrogen Energy 45, no. 7 (2020): 4991–5001. http://dx.doi.org/10.1016/j.ijhydene.2019.12.063.

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10

Bildsten, Lars. "Explosions on a Variety of Scales." Proceedings of the International Astronomical Union 7, S285 (2011): 71. http://dx.doi.org/10.1017/s1743921312000257.

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SummaryThe theoretical community is beginning to appreciate (and predict) the potential diversity of explosive outcomes from stellar evolution, while the supernovæ surveys are finding new kinds of supernovæ. This talk described two such new supernovæ. The first are ultraluminous core collapse supernovæ with radiated energies approaching 1051 ergs. The talk went on to present our recent work that explains these events with late-time energy deposition from rapidly rotating, highly magnetized neutron stars: magnetars. It concluded with our theoretical work on helium shell detonations on accreting
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Dissertationen zum Thema "Rotating Detonations"

1

Geller, Alexander C. "Thermal Imaging of RDCs and the Characterization of an Operating Map for a Novel RDC Geometry." University of Cincinnati / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin161368598622062.

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2

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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3

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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St, George Andrew. "Development and Testing of Pulsed and Rotating Detonation Combustors." University of Cincinnati / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893231.

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5

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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6

Jodele, Justas B. "Impacts of Geometrical Variations on Rotating Detonation Combustors and Pulsejets." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1560866939025106.

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7

Raj, Piyush. "Influence of Fuel Inhomogeneity and Stratification Length Scales on Detonation Wave Propagation in a Rotating Detonation Combustor (RDC)." Thesis, Virginia Tech, 2021. http://hdl.handle.net/10919/103185.

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The detonation-based engine has the key advantage of increased thermodynamic efficiency over the traditional constant pressure combustor. These detonation-based engines are also known as Pressure Gain Combustion systems (PGC) and Rotating Detonation Combustor (RDC) is a form of PGC, in which the detonation wave propagates azimuthally around an annular combustor. Prior researchers have performed a high fidelity 3-D numerical simulation of a rotating detonation combustor (RDC) to understand the flow physics such as detonation wave velocity, pressure profile, wave structure; however, performing t
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Knight, Ethan. "Effect of Corrugated Outer Wall On Operating Regimes of Rotating Detonation Combustors." University of Cincinnati / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1523631068586522.

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9

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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10

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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Bücher zum Thema "Rotating Detonations"

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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2

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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Buchteile zum Thema "Rotating Detonations"

1

Wen, Haocheng, Qiaofeng Xie, and Bing Wang. "Instabilities of Rotating Detonation." In 31st International Symposium on Shock Waves 1. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91020-8_34.

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2

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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3

Anand, Vijay, and Ephraim Gutmark. "Types of Low Frequency Instabilities in Rotating Detonation Combustors." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-98177-2_13.

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4

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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5

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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6

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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7

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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8

Zhou, R., B. L. Tian, X. P. Li, and J. P. Wang. "Large Eddy Simulation of Mixing Characteristic in the Cold Rotating Detonation Chamber." In 31st International Symposium on Shock Waves 2. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-319-91017-8_13.

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9

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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10

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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Konferenzberichte zum Thema "Rotating Detonations"

1

Rezzag, Taha, Robert Burke, and Kareem Ahmed. "A Kinematic Study of Individual Rotating Detonation Engine Waves Using K-means Algorithm." In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-58814.

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Abstract The current research is concerned with studying the instantaneous properties of the detonation waves in a RDRE by tracking each individual wave and recording its position, velocity, and peak intensity as it travels around the annulus. This information is retrieved by a non-intrusive method consisting of using a data mining technique, the k-means algorithm, to distinguish each detonation from each other in a particular frame. An algorithm was then developed to match the detonations of a current frame to the ones of a previous frame. The code was validated against results found from the
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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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Sato, Takuma, Stephen Voelkel, and Venkat Raman. "Detailed Chemical Kinetics Based Simulation of Detonation-Containing Flows." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-75878.

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Reliable and robust simulations of detonations in inhomogeneous and turbulent environments are of direct importance in the design of rotating detonation engines (RDEs). In particular, computational models will be especially useful in designing and optimizing discrete injectors that introduce fuel and air separately into the detonation chamber, but ensure appropriate level of mixing to sustain detonations but minimize backflow of detonation products and pressure waves into the feed plenums. Since the structure of detonations itself is non-ideal, models have to include a detailed description of
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FOTIA, M. L., J. HOKE, A. J. OLSON, and S. A. SCHUMAKER. "PROPAGATION OF GASEOUS DETONATIONS IN PLANAR CURVED RECTANGULAR CHANNELS." In 12TH INTERNATIONAL COLLOQUIUM ON PULSED AND CONTINUOUS DETONATIONS. TORUS PRESS, 2020. http://dx.doi.org/10.30826/icpcd12a09.

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The propagation of gaseous detonations through curved channels has a number of practical engineering applications that range from combustion initiation concepts to informing the design of rotating detonation engines. Understanding the failure mechanisms that do not allow a steadily propagating cellular detonation to traverse a curved segment of channel leads directly into these applications.
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PANIAGUA, G., J. BRAUN, T. MEYER, V. ATHMANATHAN, and S. ROY. "AN OASIS OF PURE AEROTHERMAL DILEMMAS: INTEGRATING TURBINES WITH ROTATING DETONATION COMBUSTORS." In 12TH INTERNATIONAL COLLOQUIUM ON PULSED AND CONTINUOUS DETONATIONS. TORUS PRESS, 2020. http://dx.doi.org/10.30826/icpcd12a27.

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Small Brayton/Joule engines, operating at low pressure ratios, with relatively large gap clearances exhibit poor efficiency. Instead, the development of a small rotating detonation engine holds great promise to offer mankind a sustainable solution for off-grid power generation as well as distributed systems.
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Muraleetharan, Kavi, Marc D. Polanka, Larry P. Goss, and Riley Huff. "Temperature Response of Rotating Detonations using Thin-Filament Pyrometry." In AIAA Propulsion and Energy 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-3854.

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7

Gaetano, Alec R., Vijay Anand, Jorge J. Betancourt, et al. "Tomographic Imaging of Rotating Detonations in a Hollow Combustor." In AIAA Propulsion and Energy 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-3653.

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Saha, Pankaj, Pete Strakey, and Donald Ferguson. "Numerical Investigations of Instabilities in a Natural Gas-Air Fueled Rotating Detonation Engine." In ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gt2019-91643.

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Abstract Recent numerical and experimental studies of Rotating Detonation Engines (RDEs) using air as the oxidizer have primarily focused on the ability to sustain a stable continuous detonation wave when fueled with hydrogen. For RDEs to be a viable technology for land-based power generation it is necessary to explore the ability to detonate natural gas and/or coal-syngas with air in the confines of the annular geometry of an RDE. There are major challenges in obtaining a stable detonation wave for a natural gas–air fueled RDE and to a lesser extent for coal-syngas and air. Recently published
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Saha, Pankaj, Peter Strakey, Donald Ferguson, and Arnab Roy. "Numerical Analysis of Detonability Assessment in a Natural Gas-Air Fueled Rotating Detonation Engine." In ASME 2019 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/imece2019-11728.

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Abstract Rotating Detonation Engines (RDE) offer an alternative combustion strategy to replace conventional constant pressure combustion with a process that could produce a pressure gain without the use of a mechanical compressor. Recent numerical and experimental publications that consider air as the oxidizer have primarily focused on the ability of these annular combustors to sustain a stable continuous detonation wave when fueled by hydrogen. However, for this to be a viable consideration for the land-based power generation it is necessary to explore the ability to detonate natural gas and
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Wiggins, Rachel, Alec Gaetano, Tyler Pritschau, et al. "Rotating Detonations through Hydrogen-Air and Ethylene-Air Mixtures in Hollow and Flow-Through Combustors." In AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-0420.

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Berichte der Organisationen zum Thema "Rotating Detonations"

1

Biss, Matthew M., and Kimberly Y. Spangler. Detonation Velocity Measurements from a Digital High-speed Rotating-mirror Framing Camera. Defense Technical Information Center, 2012. http://dx.doi.org/10.21236/ada576397.

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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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Stout, Jeffrey B., and Dr Edward D. Lynch. Rotating Detonation Combustion for Gas Turbines – Modeling and System Synthesis to Exceed 65% Efficiency Goal – Phase II. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1582413.

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