Trailing-Edge Flaps for Rotor Performance Enhancement and Vibration Reduction-Reference-Cited by-同舟云学术

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Trailing-Edge Flaps for Rotor Performance Enhancement and Vibration Reduction

Published:2013-04-01 Issue:2 Volume:58 Page:1-13
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:J Am Helicopter Soc

Author:

Ravichandran Kumar,Chopra Inderjit,Wake Brian E.,Hein Benjamin

Publisher

American Helicopter Society

Cited by 22 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. Interference mechanism of trailing edge flap shedding vortices with rotor wake and aerodynamic characteristics;Chinese Journal of Aeronautics;2024-08

2. Rotor Power Savings and Pitch-Link Load Reductions with Spanwise-Varying Active Camber Morphing;Journal of Aircraft;2024-05

3. A Comprehensive Study on the Aerodynamic Characteristics of Electrically Controlled Rotor Using Lattice Boltzmann Method;Aerospace;2023-11-28

4. A Study on Influence of Flapping Dynamic Characteristics on Vibration Control of Active Rotor with Trailing-Edge Flaps;Aerospace;2023-08-31

5. Parameter Analysis of Active Flap Control for Rotor Aerodynamic Control and Design;International Journal of Aerospace Engineering;2023-06-29

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