International Journal For Multidisciplinary Research

E-ISSN: 2582-2160   •   Impact Factor: 9.24

A Widely Indexed Open Access Peer Reviewed Multidisciplinary Bi-monthly Scholarly International Journal

Call for Paper Volume 6 Issue 6 November-December 2024 Submit your research before last 3 days of December to publish your research paper in the issue of November-December.
Submit Research Paper Join as a Reviewer

Plagiarism is checked by the leading plagiarism checker TurnItIn

Call for Paper

Volume 6 Issue 6
November-December 2024

Submit your research paper

Indexing Partners
Academia Advanced Sciences Index Bielefeld Academic Search Engine CiteSeer DRJI Google Scholar Independent Search Engine & Directory Network ISI (International Scientific Indexing) Issuu Mendeley Research Networks
RefSeek ResearcherId - Thomson Reuters ResearchGate Scirus Scribd Semantic Scholar UTeM - Universiti Teknikal Malaysia Melaka Wiki for Call for Papers WorldCat Zenodo

Design Optimization Of Airframe In Aircraft Fuselage Structure Under Static Loading Conditions

Author(s) Sowmya R, Sreenivasa R, Kallesh S S
Abstract The fuselage is one of the main component in any aircraft and its function is to hold all parts together and carries passengers. This fuselage part experience a different loads like static, fatigue, dynamic, buckling during landing, flying and take-off conditions. Now a day’s aircraft undergo different type of failure modes, due to improper design, pilot error, weather conditions etc. In the present work, fuselage component with airframes can be optimized in design in order to check which design of airframes in fuselage structure can withstand static loading conditions with minimum deflection and minimum induced stress. The result shows that fuselage component with airframes containing three vertical truss members under roof can able to withstand static loading conditions with minimum deflection, fuselage component with airframes containing two inclined and one vertical truss member located at centre under roof can able to withstand static loading conditions with minimum induced stress and fuselage component with airframes don’t containing any truss members under roof cannot able to withstand static loading conditions.
Keywords Fuselage, airframe, truss members, static loads
Field Physics > Mechanical Engineering
Published In Volume 1, Issue 3, November-December 2019
Published On 2019-11-09
Cite This Design Optimization Of Airframe In Aircraft Fuselage Structure Under Static Loading Conditions - Sowmya R, Sreenivasa R, Kallesh S S - IJFMR Volume 1, Issue 3, November-December 2019.
View / Download PDF File

Share this



E-ISSN 2582-2160
CrossRef

CrossRef DOI is assigned to each research paper published in our journal.

IJFMR DOI prefix is
10.36948/ijfmr

Downloads
Research Paper Format Copyright Permission Form and Undertaking Form Cover Page Vol 6 Isu 6Cover Page Vol 6 Isu 5Cover Page Vol 6 Isu 4

All research papers published on this website are licensed under Creative Commons Attribution-ShareAlike 4.0 International License, and all rights belong to their respective authors/researchers.

CC-BY-SA Open Access

About IJFMR
Fees & Payment
Current Issue
Publication Archive 		Submit Research Paper
Track Submission Status
Publication Guidelines
Publication Ethics
Peer Review & Plagiarism 		Join as a Reviewer
Editors & Reviewers
Reviewer Referral Program
Get Reviewer Membership Certi. 		Website/Journal Policies
Usage Policy
Content Policies
Privacy Policy
Contact Us +91-9898-5948-55 editor@ijfmr.com