Open Access
Issue
JNWPU
Volume 44, Number 2, April 2026
Page(s) 317 - 326
DOI https://doi.org/10.1051/jnwpu/20264420317
Published online 12 June 2026
  1. GEORGE A Bobula, RONALD H Soeder, LEO A Burkardt. Effect of variable guide vanes on the performance of a high-bypass turbofan engine[J]. Journal of Aircraft. 1983, 20(4): 306–311 [Article]. [Google Scholar]
  2. DONG Yukui, ZHAO Quanchun. Experimental study on performance optimization of fan with variable camber zero-stage guide vanes[J]. Aeroengine. 1996(3): 27–29. (in Chinese) [Google Scholar]
  3. LIN Zuoming. World aviation engine handbook[M]. Beijing: AVIC Publishing Media Co., Ltd., 2012. (in Chinese) [Google Scholar]
  4. CROUSE J E, STEINKE R J. Preliminary analysis of the effectiveness of variable geometry guide vanes to control rotor-inlet flow conditions[R]. NASA-TN-D-3823, 1967. [Google Scholar]
  5. BOHNE A, NIEHUIS R. Experimental off-design investigation of unsteady secondary flow phenomena in a three-stage axial compressor at 68% nominal speed[C]//Proceedings of the ASME Turbo Expo 2004: Power for Land, Sea, and Air, New York, 2004. [Google Scholar]
  6. DARBE R, FALK E, GORRELL S. Computational investigation of IGV-rotor interaction in turbomachinery[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2004: 3757. [Google Scholar]
  7. HÄNDEL D, BARTHMES S, NIEHUIS R, et al. u2D investigation of the flow through a symmetric variable inlet guide vane, part 1: experimental analysis[C]//49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013. [Google Scholar]
  8. HÄNDEL D, NIEHUIS R, ROCKSTROH U. Aerodynamic investigations of a variable inlet guide vane with symmetric profile[C]//Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, 2014. [Google Scholar]
  9. JI Chunjun, FAN Zhaoyang, ZHANG Yang, et al. Research on the airfoil of adjustable inlet guide vanes for a centrifugal compressor[J]. Journal of Thermal Science and Technology. 2013, 12(2): 131–134. (in Chinese) [Google Scholar]
  10. JI Chunjun, SUN Qi, FAN Zhaoyang, et al. Further research on the airfoil of inlet guide vanes for centrifugal compressors[J]. Journal of Thermal Science and Technology. 2016, 15(5): 386–390. (in Chinese) [Google Scholar]
  11. SINGH P, CHAND D S. VIGV angle optimization for subsonic axial flow compressor[J]. INCAS Bulletin. 2020, 12(2): 217–228 [Article]. [Google Scholar]
  12. SONG Junnan, GONG Jieming, LIU Yiteng, et al. Research on the influence of adjustable guide vanes on the performance of air suspension centrifugal compressors and systems[J]. Refrigeration and Air Conditioning. 2023, 37(2): 202–209. (in Chinese) [Google Scholar]
  13. WU Dong, JIN Donghai, CAO Zhipeng, et al. Influence of variable camber guide vanes on aerodynamic performance of a high-load two-stage fan[J]. Journal of Aerospace Power. 2014, 29(12): 2973–2979. (in Chinese) [Google Scholar]
  14. RAJESH E, ROY B. Numerical study of variable camber inlet guide vane on low speed axial compressor[C]//Proceedings of the ASME 2015 Gas Turbine India Conference, 2015. [Google Scholar]
  15. LU XiaoYAN Ming. Influence of variable camber guide vanes on aerodynamic performance of a 1.5-stage compressor[J]. Turbine Technology. 2018, 60(6): 407–410. (in Chinese) [Google Scholar]
  16. LIU Bo, ZHANG Guochen, WU Xiaoxiong, et al. Application of adjustable camber inlet guide vanes in counter-rotating compressors[J]. Journal of Aerospace Power. 2015, 30(5): 1184–1191. (in Chinese) [Google Scholar]
  17. LEI Peng, JIN Donghai, GUI Xingmin. Application of front and rear adjustable variable camber guide vanes in high-load fan[J]. Journal of Aerospace Power. 2019, 34(1): 177–188. (in Chinese) [Google Scholar]
  18. LIU Taiqiu, ZHAO Yuezhen, WANG Yongmei, et al. Design and experimental study on high-load single-stage axial compressor with load coefficient of 0.5[J]. Aeroengine. 2022, 48(5): 1–39. (in Chinese) [Google Scholar]
  19. ZHONG Jingjun, WANG Yuan, ZHAO Ao, et al. Influence of tip winglet on stability margin of Stage37 compressor stage[J]. Journal of Aerospace Power. 2025, 40(3): 20230349. (in Chinese) [Google Scholar]
  20. ZHONG Jingjun, ZHAO Ao, HU Yi, et al. Influence of tip winglet on stable operating margin of transonic compressor stage[J]. Journal of Aerospace Power. 2024, 39(1): 115–126. (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.