Open Access
Volume 41, Number 2, April 2023
Page(s) 363 - 369
Published online 07 June 2023
  1. XU Wenfeng, Sun Peng, YANG Guogang, et al. Numerical research on inlet total pressure distortion in a transonic compressor with non-axisymmetric stator clearance[J]. Journal of Thermal Science, 2020, 29: 893–905. [Article] [NASA ADS] [CrossRef] [Google Scholar]
  2. HOU Minjie, YE Wei, PENG Shenghong. Investigation on compatibility of future inlet/engine[J]. Aeronautical Science and Technology, 2012, 2(5): 5–8. [Article] (in Chinese) [Google Scholar]
  3. DAI Bing, YE Wei. Comparison and analysis of aeroengine stability standards between the United States and Russia[J]. Aeronautic Standardization & Quality, 2009, 21(2): 44–48 (in Chinese) [Google Scholar]
  4. XUE Haibo. Numerical simulation and parametric analysis of the distorted flow field after inserting the plate[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2008 (in Chinese) [Google Scholar]
  5. YAN Wei. Research and application of mathematic model for aerodynamic stability analysis on aviation engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016 (in Chinese) [Google Scholar]
  6. DING Ning. Inlet total pressure distortion modeling and stability analysis of high bypass ratio turbofan engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015 (in Chinese) [Google Scholar]
  7. LI Wenlan, HUANG Zhitao, QIAO Weiyang. Design and validation of simulation screen for inlet flow distortion[J]. Acta Aeronauticaet Astronautica Sinica, 1994, 15(6): 658–664. [Article] (in Chinese) [Google Scholar]
  8. BEALE D K, CRAMER K B, KINGKANA Dr P S. Development of improved methods for simulating aircraft inlet distortion in turbine engine ground tests[C]//22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2022 [Google Scholar]
  9. FANG Boyang, QIANG Xiaoqing. Design of aircraft engine inlet radial distortion generator[C]//Proceedings of the International Conference on Aerospace System Science and Engineering, Singapore, 2021: 175–186 [Google Scholar]
  10. BERNHARD H Anderson, JAMES Gibb. Vortex-generator installation studies on steady-state and dynamic distortion[J]. Journal of Aircraft, 1998, 35(4): 513–520. [Article] [CrossRef] [Google Scholar]
  11. HU Jun, ZHAO Yunsheng, DING Ning, et al. Investigation of influence of inlet distortion on high bypass ratio turbofan engine stability[J]. Aeroengine, 2013, 39(6): 6–12. [Article] (in Chinese) [Google Scholar]
  12. ZHANG Sheng, REN Wencheng, TU Baofeng, et al. CFD numerical simulating investigation on distortion net[J]. Journal of Shenyang Aerospace University, 2013, 30(5): 27–32. [Article] (in Chinese) [Google Scholar]
  13. ZHU Xudong. Comparison, improvement and application of turbulence models[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2005 (in Chinese) [Google Scholar]
  14. BU Juanjuan. Study on the flow resistance and interference of porous media[D]. Inner Mongolia: Inner Mongolia University of Science & Technology, 2020 (in Chinese) [Google Scholar]
  15. LEE K, LEE B, KANG S, et al. Inlet distortion test with gas turbine engine in the altitude engine test facility[C]//27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Chicago, 2010 [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.