TY - JOUR
T1 - Experimental study on the effect of fuel supply methods on pulse detonation combustor performance
AU - Wang, Dingding
AU - Zheng, Longxi
AU - Yang, Yudong
AU - Wang, Bowen
N1 - Publisher Copyright:
Copyright © 2025. Published by Elsevier Masson SAS.
PY - 2026/1
Y1 - 2026/1
N2 - Pulse Detonation Combustors (PDCs) represent a transformative propulsion technology capable of achieving substantial thermodynamic efficiency gains through constant-volume combustion and self-pressurization. However, conventional adaptive fuel supply methods remain fundamentally limited by their passive coupling with chamber dynamics, resulting in uncontrolled injection during critical phases such as deflagration-to-detonation transition (DDT) and exhaust. To overcome these limitations, this study introduces an actively controlled low-pressure intermittent fuel supply system, systematically examining its performance relative to conventional adaptive fueling in a gasoline/air U-bend PDC. Experimental results confirm stable detonation across 10–30 Hz under both strategies, yet the intermittent method significantly shortens the DDT distance from 733 mm to 616 mm with increasing frequency. Moreover, it enables precise temporal fuel management, yielding an 8–14 % reduction in fuel consumption while maintaining detonation stability. A notable innovative finding is the consistently shorter and stable blue flame observed at the combustor outlet under intermittent supply, indicating more complete combustion and enhanced energy release—a direct result of suppressed over-rich mixture formation during non-optimal cycles. These results underscore the critical role of active injection synchronization in detonation cycle optimization and provide a theoretical basis for advanced control strategies in next-generation PDCs.
AB - Pulse Detonation Combustors (PDCs) represent a transformative propulsion technology capable of achieving substantial thermodynamic efficiency gains through constant-volume combustion and self-pressurization. However, conventional adaptive fuel supply methods remain fundamentally limited by their passive coupling with chamber dynamics, resulting in uncontrolled injection during critical phases such as deflagration-to-detonation transition (DDT) and exhaust. To overcome these limitations, this study introduces an actively controlled low-pressure intermittent fuel supply system, systematically examining its performance relative to conventional adaptive fueling in a gasoline/air U-bend PDC. Experimental results confirm stable detonation across 10–30 Hz under both strategies, yet the intermittent method significantly shortens the DDT distance from 733 mm to 616 mm with increasing frequency. Moreover, it enables precise temporal fuel management, yielding an 8–14 % reduction in fuel consumption while maintaining detonation stability. A notable innovative finding is the consistently shorter and stable blue flame observed at the combustor outlet under intermittent supply, indicating more complete combustion and enhanced energy release—a direct result of suppressed over-rich mixture formation during non-optimal cycles. These results underscore the critical role of active injection synchronization in detonation cycle optimization and provide a theoretical basis for advanced control strategies in next-generation PDCs.
KW - Adaptive Fuel Supply
KW - Deflagration-to-Detonation Transition (DDT)
KW - Intermittent Fuel Supply
KW - Pulse Detonation Combustor
UR - https://www.scopus.com/pages/publications/105022851234
U2 - 10.1016/j.ast.2025.111329
DO - 10.1016/j.ast.2025.111329
M3 - 文章
AN - SCOPUS:105022851234
SN - 1270-9638
VL - 168
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 111329
ER -