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-Reference-Cited by-同舟云学术

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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

Published:2024-06 Issue: Volume:149 Page:109142
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

Reference44 articles.

1. Aerodynamic and acoustic analysis of helicopter main rotor blade tips in hover;Garipova;Int. J. Numer. Method. H.,2016

2. A new blade tip geometry to improve aerodynamic performance and acoustic noise of helicopter blade in hovering flight;Afshari;Aerosp. Sci. Technol.,2023

3. Experimental and theoretical studies on helicopter blade tips at ONERA;Philippe,1980

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

5. Effect of an anhedral sweptback tip on the performance of a helicopter rotor;Desopper,1987

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