Open Access
Volume 37, Number 2, April 2019
Page(s) 361 - 368
Published online 05 August 2019
  1. GohardaniA S, DoulgerisG D, SinghR. Challenges of Future Aircraft Propulsion:a Review of Distributed Propulsion Technology and Its Potential Application for the All Electric Commercial Aircraft[J]. Progress in Aerospace Sciences, 2011, 47369–391 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  2. KongXianghao, ZhangZhuoran, LuJiawei, et al. Review of Electric Power System of Distributed Electric Propulsion Aircraft Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 021651 (in Chinese) [Article] [Google Scholar]
  3. HuangJun, YangFengtian. Development and Challenges of Electric Aircraft with New Energies Acta Aeronautica et Astronautica Sinica, 2016, 37(1): 57–68 (in Chinese) [Article] [Google Scholar]
  4. Christie R J, Dubois A, Derlaga J M. Cooling of Electric Motors Used for Propulsion on SCEPTOR[R]. NASA-TM-2017-219134 [Google Scholar]
  5. Patterson M D, Derlaga J M, Borer N K, et al. High-lift Propeller System Configuration Selection for NASA's SCEPTOR Distributed Electric Propulsion Flight Demonstrator[R]. AIAA-2016-3922 [Google Scholar]
  6. Borer N K, Patterson M D, Viken J K, et al. Design and Performance of the NASA SCEPTOR Distributed Electric Propulsion Flight Demonstrator[R]. AIAA 2016-3920 Washington, 2016 [Google Scholar]
  7. Stoll A M, Bevirt J, Moore M D, et al. Drag Reduction through Distributed Electric Propulsion[R]. AIAA-2014-2851 [Google Scholar]
  8. Patterson M D, Borer N K. Approach Considerations in Aircraft with High-Lift Propeller Systems[R]. AIAA-2017-3782 [Google Scholar]
  9. Veldhuis L L M, Luursema G W. Comparison of an Actuator Disk and a Blade Modeling Approach in Navier-Stokes Calculations on the SR-3 Propfan[R]. AIAA 2000-4528, Denver, 2000 [Google Scholar]
  10. LiBo, LiangDewang, HuangGuoping. Propeller Slipstream Effects on Aerodynamic Performance of Turbo-Prop Airplane Based on Equivalent Actuator Disk Model Acta Aeronautica et Astronautica Sinica, 2008, 29(4): 845–852 (in Chinese) [Article] [Google Scholar]
  11. ZuoSuihan, YangYong. Numerical Simulation of Propeller/High-Lift System Interaction Aeronautical Computing Technique, 2007, 37(1): 54–57 (in Chinese) [Article] [Google Scholar]
  12. XiaZhenfeng, LuoSong, YangYong. Numerical Simulations of Propeller Slipstream Flows Using Actuator Disk Theory Acta Aerodynamica Sinica, 2012, 30(2): 219–222 (in Chinese) [Article] [Google Scholar]
  13. YangXiaochuan, WangYuntao, WangGuangxue. Numerical Simulation of Propeller Slipstream Based on Equivalent Actuator Disk Model Physics of Gases Theory and Applications, 2012, 7(3): 40–47 (in Chinese) [Article] [Google Scholar]
  14. ZhangXiaoli, ZhangYifan. Research on Interaction of Propeller and High-Lift System Aeronautical Computing Technique, 2011, 41(4): 1–3 (in Chinese) [Article] [Google Scholar]
  15. Roosenboom E W M, Sturmer A, Schroder A. Comparison of PIV Measurements with Unsteady Rans Calculations in a Propeller Slipsteam[R]. AIAA-2009-3626 [Google Scholar]
  16. ZhangLiu, BaiJunqiang, LiHuaxing, et al. Research on Aerodynamic Interference for Propeller Slipstream over the Wing Aeronautical Computing Technique, 2012, 42(2): 87–91 (in Chinese) [Article] [Google Scholar]
  17. XuHeyong, YeZhenyin. Numerical Simulation of Unsteady Propeller Slipstream Journal of Aerospace Power, 2011, 26(1): 148–153 (in Chinese) [Article] [Google Scholar]
  18. YangXiaochuan, WangYuntao, WangGuangxue, et al. Numerical Simulation of Unsteady Propeller Slipstream ACTA Aerodynamica Sinica, 2014, 32(3): 289–294 (in Chinese) [Article] [Google Scholar]
  19. WangWei, DuanZhuoyi, GengJianzhong, et al. Aerodynamics Analysis of Two-Turboprop Aircraft with Propeller Slipstream Effects Considered Journal of Northwestern Polytechnical University, 2017, 35(6): 1105–1110 (in Chinese) [Article][Article] [Google Scholar]
  20. WangYuntao, WangGuangxue, ZhangYulun. Drag Prediction of DLR-F6 Configuration with TRIP2.0 Software Acta Aerodynamica Sinica, 2009, 27(1): 108–113 (in Chinese) [Article] [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.