|
|||||||||||||||
|
INTERNATIONAL JOURNAL OF NOVEL RESEARCH AND DEVELOPMENT International Peer Reviewed & Refereed Journals, Open Access Journal ISSN Approved Journal No: 2456-4184 | Impact factor: 8.76 | ESTD Year: 2016 Scholarly open access journals, Peer-reviewed, and Refereed Journals, Impact factor 8.76 (Calculate by google scholar and Semantic Scholar | AI-Powered Research Tool) , Multidisciplinary, Monthly, Indexing in all major database & Metadata, Citation Generator, Digital Object Identifier(DOI) |
||||||||||||||
Issue: April 2024
Volume 9 | Issue 4
Review Result and Publication of Paper within : 2-3 days
Click Here For more DetailsFor Authors
Forms / Download
Published Issue Details
Editorial Board
Other IMP Links
Facts & Figure
Impact Factor : 8.76
Issue per Year : 12
Volume Published : 9
Issue Published : 95
Article Submitted :
Article Published :
Total Authors :
Total Reviewer :
Total Countries :
Indexing Partner
Join RMS/Earn 300
Licence
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
|
Published Paper Details
|
|
| Paper Title: | OPTIMAL DESIGN OF ROTOR HUB FOR DIFFERENT MATERIALS |
| Authors Name: | Dr J.V.R.Ramesh , K.Yogesh |
| Download E-Certificate: | Download |
| Author Reg. ID: |
IJNRD_170158
|
| Published Paper Id: | IJNRD1711010 |
| Published In: | Volume 2 Issue 11, November-2017 |
| DOI: | |
| Abstract: | The rotor system is the revolving part of a helicopter which generates lift. This rotor consists of a mast, rotor blades, and hub. The mast is a hollow cylindrical metal shaft which extends in an upward direction from and is driven. Sometimes it is supported by the transmission also. On the top, a mast is the attachment point for the rotor blades (hub). The rotor blades are attached to the hub by different methods. Critical rotor systems are classified according to how they move relative to the main rotor hub and how the main rotor blades are attached. As the rotor starts spinning, each blade responds to inputs from the control system to enable helicopter control. The centre of lift on the whole rotor system proceeds in response to these inputs to impact pitch, roll, and move in upward motion. In this case, the rotor hub must carry aerodynamic forces and the blade weight as rotational speeds. For that of helicopter rotor hub strength will be calculated. In this project, the 3d model of helicopter main rotor hub shall be done in Unigraphics and imported into ansys software to perform static analysis to analyze the strength of rotor hub and optimize by using different materials. |
| Keywords: | OPTIMAL DESIGN OF ROTOR HUB FOR DIFFERENT MATERIALS |
| Cite Article: | "OPTIMAL DESIGN OF ROTOR HUB FOR DIFFERENT MATERIALS ", International Journal of Novel Research and Development (www.ijnrd.org), ISSN:2456-4184, Vol.2, Issue 11, page no.60-63, November-2017, Available :http://www.ijnrd.org/papers/IJNRD1711010.pdf |
| Downloads: | 000118753 |
| ISSN: |
2456-4184 | IMPACT FACTOR: 8.76 Calculated By Google Scholar| ESTD YEAR: 2016 An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 8.76 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator |
| Publication Details: |
Published Paper ID:IJNRD1711010 Registration ID: 170158 Published In: Volume 2 Issue 11, November-2017 DOI (Digital Object Identifier): Page No: 60-63 Country: -, -, -- Research Area: Engineering Publisher : IJ Publication Published Paper URL : https://www.ijnrd.org/viewpaperforall?paper=IJNRD1711010 Published Paper PDF: https://www.ijnrd.org/papers/IJNRD1711010 |
| Share Article: |
|
|
Click Here to Download This Article |
|
| Article Preview | |
|
|
|
Major Indexing from www.ijnrd.org
| Semantic Scholar | Microsaoft Academic | ORCID | Zenodo |
| Google Scholar | ResearcherID Thomson Reuters | Mendeley : reference manager | Academia.edu |
| arXiv.org : cornell university library | Research Gate | CiteSeerX | PUBLON |
| DRJI | SSRN | Scribd | DocStoc |
ISSN Details
 |
 |
|
ISSN: 2456-4184
Impact Factor: 8.76 and ISSN APPROVED
Journal Starting Year (ESTD) : 2016
DOI (A digital object identifier)
Conference
Open Access License Policy
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
Important Details
Social Media
Licence
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
Join RMS/Earn 300
| Copyright © 2024 - All Rights Reserved - IJNRD |
Facebook Twitter Instagram LinkedIn