A new blade tip geometry to improve aerodynamic performance and acoustic noise of helicopter blade in hovering flight-Reference-Cited by-同舟云学术

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A new blade tip geometry to improve aerodynamic performance and acoustic noise of helicopter blade in hovering flight

Published:2023-04 Issue: Volume:135 Page:108197
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Afshari Reza,Karimian S.M.H.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Rotorcraft Aeromechanics;Johnson,2013

2. Aerodynamic shape of the wing tips;Hoerner,1949

3. Experimental investigation of model variable Geometry and ogee tip rotors;Landgrebe,1974

4. Influence of tip shape, chord, blade number, and airfoil on advanced rotor performance;McVeigh;J. Am. Helicopter Soc.,1984

5. Special vortices at a helicopter rotor blade;Müller;J. Am. Helicopter Soc.,1990

Cited by 3 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. Numerical investigation on the use of various blade tips for the helicopter's main rotor blade in forward flight regarding aerodynamic performance and HSI noise considerations;Aerospace Science and Technology;2024-06

2. Modeling and free vibration analysis of a rotating functionally graded thin-walled hub-blade system under aerothermoelastic loading;Aerospace Science and Technology;2024-03

3. Investigation of Helicopter Blade Tip Configuration during Hover Flight Employing Computational Fluid Dynamics;Modelling and Simulation in Engineering;2024-01

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