CONCEPTUAL DESIGN OF 180-SEATER PASSENGER AIRCRAFT

  • Unique Paper ID: 144888
  • Volume: 4
  • Issue: 6
  • PageNo: 73-81
  • Abstract:
  • This paper presents a study on conceptual design of a 180-seater medium range passenger aircraft. The main purpose is to understand the importance of aircraft design, the steps involved, and the parameters considered in designing an aircraft with specified mission. The design point is considered by historical data of similar range aircraft- by comparing their weights, powerplants used, cruising altitude and speed, service ceiling, and geometrical dimensions of aircraft body. The aircraft will possess a low wing, tricycle landing gear, and a conventional tail arrangement. After the design calculations are complete, the geometry of the aircraft is generated using CATIA V5R20.

Copyright & License

Copyright © 2025 Authors retain the copyright of this article. This article is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

BibTeX

@article{144888,
        author = {Shahid Ameen Khan and Kruthika H. V and Vinay M. R and Vigneswaran C. M},
        title = {CONCEPTUAL DESIGN OF 180-SEATER PASSENGER AIRCRAFT},
        journal = {International Journal of Innovative Research in Technology},
        year = {},
        volume = {4},
        number = {6},
        pages = {73-81},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=144888},
        abstract = {This paper presents a study on conceptual design of a 180-seater medium range passenger aircraft. The main purpose is to understand the importance of aircraft design, the steps involved, and the parameters considered in designing an aircraft with specified mission. The design point is considered by historical data of similar range aircraft- by comparing their weights, powerplants used, cruising altitude and speed, service ceiling, and geometrical dimensions of aircraft body. The aircraft will possess a low wing, tricycle landing gear, and a conventional tail arrangement. After the design calculations are complete, the geometry of the aircraft is generated using CATIA V5R20.},
        keywords = {Aircraft design, conceptual design process, performance characteristics.},
        month = {},
        }

Cite This Article

  • ISSN: 2349-6002
  • Volume: 4
  • Issue: 6
  • PageNo: 73-81

CONCEPTUAL DESIGN OF 180-SEATER PASSENGER AIRCRAFT

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