Experimental research on the performance of hollow and annular rotating detonation engines with nozzles

Y Zhang, Z Sheng, G Rong, D Shen, K Wu… - Applied Thermal …, 2023 - Elsevier
Rotating detonation engines (RDEs), which are hoped to achieve significant performance
improvements in propulsion systems, have received much attention in recent years. The …

Rotating detonation wave direction and the influence of nozzle guide vane inclination

E Bach, CO Paschereit, P Stathopoulos, MD Bohon - AIAA Journal, 2021 - arc.aiaa.org
This study describes a rotating detonation combustor (RDC) equipped with a set of nozzle
guide vanes (NGVs) of variable number and inclination angle. Different instrumented guide …

Investigation of pressure gain characteristics for kerosene-hot air RDE

J Zhou, F Song, Y Wu, S Xu, X Yang, P Cheng… - Combustion and Flame, 2023 - Elsevier
Total pressure gain is one of the most significant performance metrics for rotating detonation
engines. In this study, total pressure gains of kerosene-hot air (523K∼ 553 K) RDE for …

Advancement of empirical model for stagnation pressure gain in rdcs

E Bach, CO Paschereit, P Stathopoulos… - AIAA Scitech 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0834. vid This study describes the
experimental characterization of an RDC across a broad parameter range. The operation …

Experimental approaches for obtaining a temporally-and spatially-averaged representative static pressure for rotating detonation engines

JR Codoni, G Birindelli, A Thoeny… - AIAA Scitech 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-2369. vid The objectives of this
work are twofold. First, to present a current status of the NPS RPL effort to experimentally …

Investigation of pressure gain characteristics of RDE with Tesla valve inlet scheme

J Zhou, F Song, Y Wu, S Xu, X Yang, H Liu… - Experimental Thermal and …, 2023 - Elsevier
Total pressure gain is one of the most significant performance metrics for rotating detonation
engines. In this study, a Tesla valve is introduced with the intention of suppression of …

Evaluation of Uncertainties of Pressure Gain Measurements in Rotating Detonation Combustor

AD Feleo, M Gamba - AIAA Journal, 2024 - arc.aiaa.org
Experimentally measuring the pressure gain of a rotating detonation combustor through the
method of equivalent available pressure is prone to many experimental uncertainties. A …

Numerical and experimental evaluation of shock dividers

M Rezay Haghdoost, BS Thethy, M Nadolski, B Seo… - Shock Waves, 2022 - Springer
Mitigation of pressure pulsations in the exhaust of a pulse detonation combustor is crucial for
operation with a downstream turbine. For this purpose, a device termed the shock divider is …

Computational Assessment of the Impact of Wave Count on Rotating Detonation Engine Performance

DE Paxson - AIAA SciTech 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1290. vid The impact of the number
of azimuthally propagating waves on the performance of a Rotating Detonation Engine …

Tesla Rdc Operation and Performance

F Song, Y Wu, X Yang, J Zhou, S Xu, J Kang… - Available at SSRN … - papers.ssrn.com
The suppression of pressure feedback and the control for detonation wave operating mode
play a key role in improving the stagnation pressure gain of RDC. In this study, a unique …