UGC Approved Journal no 63975(19)

ISSN: 2349-5162 | ESTD Year : 2014
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Published in:

Volume 5 Issue 5
May-2018
eISSN: 2349-5162

UGC and ISSN approved 7.95 impact factor UGC Approved Journal no 63975

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Published Paper ID:
JETIR1805594


Registration ID:
182498

Page Number

1031-1035

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Title

Total take off weight estimation on nose wheel landing gear

Abstract

Abstract : Landing gear is the undercarriage of an aircraft or spacecraft and is often referred to as such. For aircraft, the landing gear supports the craft when it is not flying, allowing it to take off, land and usually to taxi without damage. Wheels are typically used but skids, skis, floats or a combination of these and other elements can be deployed depending both on the surface and on whether the craft only operates vertically (VTOL) or is able to taxi along the surface. Faster aircraft usually have retractable undercarriage, which folds away during flight to reduce air resistance or drag. For launch vehicles and spacecraft landers, the landing gear is typically designed to support the vehicle only post-flight, and are not used for takeoff or surface movement. There is a need to design landing gear with minimum weight, minimum volume, high performance, improved life and reduced life cycle hence, the purpose this paper is to estimate the total Take off weight of an aircraft Nose wheel landing gear. Many technologies have been developed over the years to meet these challenges. The most critical part in the landing gear is the strut. This paper presents the FEM analysis of a landing gear strut which is acted upon by landing load. __________________________________________________________

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"Total take off weight estimation on nose wheel landing gear", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.5, Issue 5, page no.1031-1035, MAY-2018, Available :http://www.jetir.org/papers/JETIR1805594.pdf

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2349-5162 | Impact Factor 7.95 Calculate by Google Scholar

An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 7.95 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator

Cite This Article

"Total take off weight estimation on nose wheel landing gear", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 5, page no. pp1031-1035, MAY-2018, Available at : http://www.jetir.org/papers/JETIR1805594.pdf

Publication Details

Published Paper ID: JETIR1805594
Registration ID: 182498
Published In: Volume 5 | Issue 5 | Year May-2018
DOI (Digital Object Identifier):
Page No: 1031-1035
Country: Mangalore, Karnataka, India .
Area: Other
ISSN Number: 2349-5162
Publisher: IJ Publication


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