Open Access
Issue
JNWPU
Volume 41, Number 6, Decembre 2023
Page(s) 1125 - 1133
DOI https://doi.org/10.1051/jnwpu/20234161125
Published online 26 February 2024
  1. FICKETT W, DAVIS W C. Detonation: theory and experiment[M]. New York: Dover Publications Inc, 2000 [Google Scholar]
  2. LU F K, BRAUN E M. Rotating detonation wave propulsion: experimental challenges, modeling, and engine conceptsJournal of Propulsion and Power 201430(5): 1125–1142 [Article] [CrossRef] [Google Scholar]
  3. WOLAÑSKI P. Detonative propulsion[J]. Proceedings of the Combustion Institute, 2013, 34(1): 125–158 [Article] [CrossRef] [Google Scholar]
  4. MUNIPALLI R, SHANKAR V, WILSON D R, et al. Preliminary design of a pulsed detonation based combined cycle engine[C]//10th International Symposium of Air Breathing Engine, 2001 [Google Scholar]
  5. KAEMMING T. Integrated vehicle comparison of turbo-ramjet engine and pulsed detonation engine[C]//Proceedings of ASME Turbo Expo, 2001 [Google Scholar]
  6. BUSSING T R A, LIDSTONE G, CHRISTOFFERSON E, et al. Pulse detonation propulsion proof of concept test article development[C]//38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2002 [Google Scholar]
  7. WANG K, FAN W. Efforts on high-frequency pulse detonation engines[J]. Journal of Propulsion and Power, 2016, 33(1): 17–28 [Google Scholar]
  8. YU Xiaodong, WANG Ke, ZHU Yiyuan et al. . Experimental study on liquid fueled high-frequency detonations in the valveless scheme[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43: 126245 (in Chinese) [Google Scholar]
  9. WANG K, WANG Z, ZHANG Q, et al. Study on a simplified double-frequency scheme for pulse detonation rocket engines[J]. Acta Astronautica, 2018, 148: 337–344 [Article] [CrossRef] [Google Scholar]
  10. LU W, FAN W, WANG K, et al. Operation of a liquid-fueled and valveless pulse detonation rocket engine at high frequency[J]. Proceedings of the Combustion Institute, 2017, 36(2): 2657–2664 [Article] [CrossRef] [Google Scholar]
  11. ANDERSON E, STEVENS C, HOKE J, et al. Ball valve pulsed detonation engine[C]//49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2011 [Google Scholar]
  12. MERCURIO N, PAL S, WOODWARD R, et al. Experimental studies of the unsteady ejector mode of a pulse detonation rocket-based combined cycle engine[C]//46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2010 [Google Scholar]
  13. WU Y, HAN Q, SHEN Y, et al. Ignition study on a rotary-valved air-breathing pulse detonation engine[J]. International Journal of Turbo & Jet-Engines, 2015, 34(2): 1–12 [Google Scholar]
  14. PENG Changxin. Investigation on key technologies of pulse detonation combustor as bypass burner[D]. Xi'an: Northwestern Polytechnical University, 2013 (in Chinese) [Google Scholar]
  15. MA Hu. Investigation on pulse detonation engine with reed valve[D]. Nanjing: Nanjing University of Science and Technology, 2015 (in Chinese) [Google Scholar]
  16. DANIAU E, FALEMPIN F, ZHANG G, et al. Preliminary work for a pulsed detonation engine demonstrator[C]//14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006 [Google Scholar]
  17. MATSUOKA K, YAGETA J, NAKAMICHI T, et al. Inflow-driven valve system for pulse detonation engines[J]. Journal of Propulsion and Power, 2011, 27(3): 597–607 [Article] [CrossRef] [Google Scholar]
  18. MATSUOKA K, ESUMI M, IKEGUCHI K B, et al. Optical and thrust measurement of a pulse detonation combustor with a coaxial rotary valve[J]. Combustion and Flame, 2012, 159(3): 1321–1338 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  19. ZHEN Dianfeng, YANG Yiyong, WANG Jiahua. Design and experimental investigation of blunt aero-valve for air-breathing pulse detonation engine[J]. Acta Scientiarum Naturalium Universitatis Pekinensis, 2012, 48(3): 347–353 (in Chinese) [Google Scholar]
  20. GONG Jishuang. Investigation on improving performance of aero-valve pulse detonation engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012 (in Chinese) [Google Scholar]
  21. YANG Guangyuan. Analysis and experimental investigation on the thrust performance of aero-valve pulse detonation engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2017 (in Chinese) [Google Scholar]
  22. QIU H, XIONG C, YAN C, et al. Effect of aerodynamic valve on backflow in pulsed detonation tube[J]. Aerospace Science and Technology, 2013, 25(1): 1–15 [Article] [CrossRef] [Google Scholar]
  23. FOA J V. Elements of flight propulsion[M]. New York and London: John Wiley & Sons, 1960 [Google Scholar]
  24. LU Jie. Investigation on key technologies of the pulse detonation turbine engine[D]. Xi'an: Northwestern Polytechnical University, 2012 (in Chinese) [Google Scholar]
  25. WANG Z, WANG Y, HUANG J, et al. Back-propagation suppression study based on intake configuration optimization for an air-breathing pulse detonation engine[J]. Aerospace Science and Technology, 2021, 118: 107042 [Article] [CrossRef] [Google Scholar]
  26. LI Qing'an, WANG Ke, SUN Tianyu, et al. Numerical study on propagation characteristics of back-pressure in a pulse detonation engine[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(1): 103–110 (in Chinese) [Google Scholar]
  27. TESLA N. Valvular Conduit: US, 1329559[P]. 1920-02-03 [Google Scholar]
  28. ZHANG Wenlong. Research on measurement and control method and implementation technology of valveless pulse detonation rocket engine[D]. Xi'an: Northwestern Polytechnical University, 2019 (in Chinese) [Google Scholar]
  29. SHA Dingguo. Error analysis and evaluation of measurement uncertainty[M]. Beijing: China Metrology Publishing House, 2003 (in Chinese) [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.