Aerodynamic prediction of helicopter rotor in forward flight using blade element theory-Reference-Cited by-同舟云学术

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Aerodynamic prediction of helicopter rotor in forward flight using blade element theory

Published:2017-06-30 Issue:2 Volume:11 Page:2711-2722
ISSN:2289-4659
Container-title:JOURNAL OF MECHANICAL ENGINEERING AND SCIENCES
language:
Short-container-title:J. MECH. ENG. SCI.

Author:

Yaakub M.F., ,Wahab A.A.,Abdullah A.,Nik Mohd N.A.R.,Shamsuddin S.S., , , ,

Publisher

Universiti Malaysia Pahang Publishing

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Fuel Technology,Computational Mechanics

Cited by 8 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. Aerodynamic Analysis of Mathematically Modelled Propeller for Small UAV Using CFD in Different Temperature Conditions;Strojniški vestnik - Journal of Mechanical Engineering;2023-11-21

2. Flight Dynamics of A ‘V’ Shape Boomerang: Effect of Wind on Boomerang Trajectory;2023 Moratuwa Engineering Research Conference (MERCon);2023-11-09

3. Numerical study of airfoil used for helicopter rotor tip to investigate the enhancement in the aerodynamic characteristics using active flow control at forward flight conditions;Journal of Physics: Conference Series;2023-11-01

4. Helicopter performance enhancement by alleviating retreating blade stall using active flow control;Scientific African;2023-09

5. Calculation of Air Velocity on the Helicopter Turboshaft Engines Inlet;SAE International Journal of Engines;2021-12-27

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