Reduction of Tiltrotor Download
Author:
Affiliation:
1. Bell Helicopter Textron Inc., Fort Worth, Texas
Publisher
American Helicopter Society
Cited by 15 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Tip Vortex Trajectory and Its Application in Small-Rotor/Wing Interaction;AIAA SCITECH 2024 Forum;2024-01-04
2. Battery Sensitivity Analysis on Initial Sizing of eVTOL Aircraft;Journal of the Korean Society for Aeronautical & Space Sciences;2022-12-31
3. Investigation of Fountain Effect in Dual-Rotor/Wing Interaction at Low Reynolds Number;AIAA AVIATION 2022 Forum;2022-06-20
4. Flap Usage Considering Swirl Velocities to Reduce the Download on a Winged Helicopter in Hover;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2022
5. Experimental and Analytical Analysis of Rotor-Wing Interaction in Hover for Low Reynolds Number Flow;Journal of Aerospace Engineering;2021-11
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