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:
JETIR18IC055


Registration ID:
181391

Page Number

281-289

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Title

Design and Analysis of wings of an aerial vehicle

Abstract

This paper details the design and analysis of a vehicle which is capable of both on-road operation and aerial travel. It was decided to design the vehicle in such a manner as to provide a feasible means of travel in regional centres and hence, reduce lengthy road travel or dependency on chartered flights. To design the airframe a classical approach was folloowed, whereby feasibility studies and statistical analysis were carried out on the development of existing flying cars and roadable aircraft. Within these analyses, two main design constraints were considered important for the commercial success of the vehicle; the handling qualities of each vehicle configuration and the ease of conversion between plane and car modes. As well as these constraints, the interior arrangement was also carefully considered. In order to address the handling issues, it was decided that the vehicle should be capable of conventional control while operating in both modes. To fulfil the desired role as a substitute vehicle for regional travel, the total mission profile was considered as driving from a residence to a nearby airport before flying to a regional airstrip and driving to the final destination. The vehicle was capable of takeoff weight 1193 kg, maximum fuel weight 219kg, and can achieve a cruise speed of 77m/s and stall speed 28m/s at altitude 2500km, with a flight range of 980km, and rate of climb 755ft/min(3.83m/s) with available thrust 645kg.

Key Words

Flying car, mission profile, takeoff weight, fuel weight, cruise, stall, range

Cite This Article

"Design and Analysis of wings of an aerial vehicle", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.5, Issue 5, page no.281-289, May-2018, Available :http://www.jetir.org/papers/JETIR18IC055.pdf

ISSN


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

"Design and Analysis of wings of an aerial vehicle", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.5, Issue 5, page no. pp281-289, May-2018, Available at : http://www.jetir.org/papers/JETIR18IC055.pdf

Publication Details

Published Paper ID: JETIR18IC055
Registration ID: 181391
Published In: Volume 5 | Issue 5 | Year May-2018
DOI (Digital Object Identifier):
Page No: 281-289
Country: Nagpur, Maharashtra, India .
Area: Engineering
ISSN Number: 2349-5162
Publisher: IJ Publication


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