ISSN: 2349-5162 | Impact Factor: 5.87

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Published in:

Volume 5 Issue 2
February-2018
eISSN: 2349-5162

Unique Identifier

JETIR1802081

Page Number

496-502

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Title

DESIGN AND OPTIMIZATION OF HELICOPTER ROTOR BLADE USING DIFFERENT MATERIALS

ISSN

2349-5162

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"DESIGN AND OPTIMIZATION OF HELICOPTER ROTOR BLADE USING DIFFERENT MATERIALS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.5, Issue 2, page no.496-502, February-2018, Available :http://www.jetir.org/papers/JETIR1802081.pdf

Abstract

The blades of a helicopter are long, limited with a secondary perspective proportion. The shapes of the blade are such-and-such minimizes drag starting with the tip of the vertices. They hold a level about messiness that lessens those lift created at the corners, the place the wind current may be speediest also vortex era. Blades of the rotor are large would commit out for different materials, such as aluminum, composites, also steel. The helicopter rotor centre is powered toward the engine, and the rotor blades would connect to the centre. The movement of sharpened steel is regulated toward the helicopter rotor framework. Those fundamental rotor sharpened steel influenced toward the wind stream for revolution about sharpened steel and the impact of aeromechanic energy and radial energy applying will be sharpened steel need to been completely acknowledged. The changing qualities dissection from claiming rotor edge is principally included in the vibration control. The goal will should figure the common recurrence furthermore operating recurrence for rotor edge may be modulating the individual’s frequencies also avoiding thunder in rotational speed, in this way, the vibrations of the helicopter might diminish. In this project, the three-dimension model of helicopter rotor blade is modeled in NX-CAD and imported into ANSYS software to analyze the strength, and dynamic characteristics of rotor blade have been developed. The static strength and the dynamic characteristics about rotor blade have been analyzed with ANSYS software for different materials (aluminum alloy and composite materials). Throughout those contemplate of changing trademark analysis, those impact of aeromechanic energy What's more radial energy applying with sharpened steel need to been completely viewed.

Key Words

DESIGN AND OPTIMIZATION OF HELICOPTER ROTOR BLADE USING DIFFERENT MATERIALS

Cite This Article

"DESIGN AND OPTIMIZATION OF HELICOPTER ROTOR BLADE USING DIFFERENT MATERIALS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 2, page no. pp496-502, February-2018, Available at : http://www.jetir.org/papers/JETIR1802081.pdf

Publication Details

Published Paper ID: JETIR1802081
Registration ID: 180299
Published In: Volume 5 | Issue 2 | Year February-2018
DOI (Digital Object Identifier):
Page No: 496-502
ISSN Number: 2349-5162

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(Volume 5 | Issue 11 | November 2018 |Impact factor 5.87)

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Cite This Article

"DESIGN AND OPTIMIZATION OF HELICOPTER ROTOR BLADE USING DIFFERENT MATERIALS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 2, page no. pp496-502, February-2018, Available at : http://www.jetir.org/papers/JETIR1802081.pdf

Important Dates Related to Publication Procedure:
  • » Paper Submission Till: 29 November 2018.
  • » UGC and ISSN Approved Journal
  • » Review (Acceptance/Rejection) Notification: Within 02-04 Days.
  • » Paper Publish:Within 02-07 Days after submitting the all documents.
  • » Frequency: Monthly (12 issue Annually)
  • » Journal Type : Open Access
  • »Indexing In Google Scholar, ResearcherID Thomson Reuters, Mendeley : reference manager, Academia.edu, arXiv.org, Research Gate, CiteSeerX, DocStoc, ISSUU, Scribd, and many more | High Impact Factor: 5.87 Digital object identifier (DOI) and Hard Copy of certificate Provided.
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Impact factor: 5.87