UGC Approved Journal no 63975

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

Volume 6 Issue 6
June-2019
eISSN: 2349-5162

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

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Unique Identifier

Published Paper ID:
JETIRDC06013


Registration ID:
221575

Page Number

77-81

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Title

Title: Aerodynamic analysis and optimisation of the futuristic Box-wing type Aircraft configuration

Abstract

A conceptual design optimization was carried out for a long-range Box-wing aircraft. A baseline conventional cantilever wing aircraft was selected for the mission requirements as baseline box wing aircraft. Lift and drag coefficients for the fore and aft wings of the box wing aircraft was calculated and compared with the conventional cantilever wing aircraft. The results indicate that the box wing aircraft would generate less induced drag and greater lift than the conventional cantilever wing aircraft. Theoretical calculations were carried out to investigate the take-off and landing distance for box wing configuration and compared to that of conventional cantilever wing. Induced drag was calculated for box wing and cantilever wing by varying the geometric parameters like aspect ratio, span, surface area and sweep angle to achieve the best possible dimensions. CFD studies were carried out to investigate the effect of stagger and gap and to optimize them. Numerical simulation was also carried out to study the static pressure and velocity distribution over the box wing. Thus, it is observed that overall flight performance of the box wing seemed to be better than the conventional cantilever wing aircraft. Box wing type of futuristic aircraft configuration seemed to be fuel efficient as compared to the conventional cantilever wing type of aircraft configuration.

Key Words

design optimization, conventional cantilever wing aircraft, box wing configuration, fuel efficient.

Cite This Article

"Title: Aerodynamic analysis and optimisation of the futuristic Box-wing type Aircraft configuration ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.77-81, June 2019, Available :http://www.jetir.org/papers/JETIRDC06013.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

"Title: Aerodynamic analysis and optimisation of the futuristic Box-wing type Aircraft configuration ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp77-81, June 2019, Available at : http://www.jetir.org/papers/JETIRDC06013.pdf

Publication Details

Published Paper ID: JETIRDC06013
Registration ID: 221575
Published In: Volume 6 | Issue 6 | Year June-2019
DOI (Digital Object Identifier):
Page No: 77-81
Country: Chennai, Tamil Nadu, India .
Area: Engineering
ISSN Number: 2349-5162


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