Open Access
Issue
JNWPU
Volume 42, Number 1, February 2024
Page(s) 149 - 156
DOI https://doi.org/10.1051/jnwpu/20244210149
Published online 29 March 2024
  1. YAN Chuanjun, FAN Wei. Theories and key technologies of the pulse detonation engine[M]. Xi'an: Northwestern Polytechnical University Press, 2005: 4–6 (in Chinese) [Google Scholar]
  2. ZHENG Longxi, WANG Zhiwu, HUANG Xiqiao, et al. Technologies of pulse detonation turbine engine[M]. Xi'an: Northwestern Polytechnical University Press, 2019: 27–28 (in Chinese) [Google Scholar]
  3. MAWID M A, PARK T W, SEKAR B. Performance analysis of a pulse detonation device as an afterburner[R]. AIAA-2000-3474 [Google Scholar]
  4. MAWID M A, PARK T W. Towards replacement of turbofan engines afterburners with pulse detonation devices[R]. AIAA-2001-3470 [Google Scholar]
  5. MAWID M A, PARK T W, SEKAR B, et al. Application of pulse detonation combustion to turbofan engines[J]. Journal of Engineering for Gas Turbines and Power, 2003, 125(1): 270–283. [Article] [Google Scholar]
  6. KUMAR S A. Parametric and performance analysis of a hybrid pulse detonation turbofan engine[D]. Arlington: The University of Texas at Arlington, 2011 [Google Scholar]
  7. CHEN Wenjuan, FAN Wei, QIU Hua, et al. Thermal performance analysis of turbofan engine with the pulse detonation combustors in the bypass duct[J]. Journal of Northwestern Polytechnical University, 2010, 28(2): 240–244. [Article] (in Chinese) [Google Scholar]
  8. CHEN Wenjuan, FAN Wei, QIU Hua, et al. Thermodynamic performance analysis of turbofan engine with a pulse detonation duct heater[J]. Aerospace Science and Technology, 2012, 23(1): 206–212. [Article] [Google Scholar]
  9. LU Jie, ZHENG Longxi, WANG Zhiwu, et al. Investigate on performance of pulse detonation turbine engine with PDC as a duct heater[J]. Journal of Propulsion Technology, 2014, 35(6): 858–864. [Article] (in Chinese) [Google Scholar]
  10. ENDO T, FUJIWARA T. Analytical estimation of performance parameters of an ideal pulse detonation engine[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2003, 45(150): 249–254. [Article] [Google Scholar]
  11. ENDO T, KASAHARA J, MATSUO A, et al. Pressure history at the thrust wall of a simplified pulse detonation engine[J]. AIAA Journal, 2004, 42(9): 1921–1930. [Article] [Google Scholar]
  12. LU Jie. Investigations on key technologies of the pulse detonation turbine engine[D]. Xi'an: Northwestern Polytechnical University, 2016: 31–40 (in Chinese) [Google Scholar]
  13. WANG Lingyi, ZHENG Longxi, HUANG Kang, et al. Operating characteristic of a reverse flow pulse detonation combustor[J]. Journal of Propulsion Technology, 2021, 42(4): 898–905. [Article] (in Chinese) [Google Scholar]
  14. LIAN Xiaochun, WU Hu. Principle of aeroengine[M]. Xi'an: Northwestern Polytechnical University Press, 2005: 243–255 (in Chinese) [Google Scholar]
  15. ZHANG Qun, HUANG Xiqiao. Combustion science of aeroengine[M]. Beijing: National Defense Industry Press, 2020: 211–212 (in Chinese) [Google Scholar]
  16. CHEN Wenjuan, ZHANG Qun, FAN Wei, et al. Experiment on wall temperature of an air-breathing pulse detonation engine[J]. Journal of Propulsion Technology, 2011, 32(2): 296–300. [Article] (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.