UGC Approved Journal no 63975(19)

ISSN: 2349-5162 | ESTD Year : 2014
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Volume 11 | Issue 7 | July 2024

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Published in:

Volume 11 Issue 6
June-2024
eISSN: 2349-5162

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Published Paper ID:
JETIR2406146


Registration ID:
542358

Page Number

b360-b373

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Title

Aerodynamics of V/STOL (Vertical/Short Takeoff and Landing) Aircraft

Authors

Abstract

This research paper delves into the unique aerodynamic principles and challenges associated with Vertical/Short Takeoff and Landing (V/STOL) aircraft. These aircraft represent a significant advancement in aviation technology, enabling operations in environments with limited runway space. The paper reviews existing literature, providing a comprehensive overview of the current state of V/STOL technology. It discusses the technical aspects and design considerations, including lift and thrust mechanisms, control surfaces, transition phases, hovering capabilities, and drag reduction strategies. Key findings highlight the complexities involved in balancing weight, developing efficient propulsion systems, ensuring structural integrity, and mitigating noise and vibration. Through detailed case studies of notable V/STOL aircraft such as the Harrier Jump Jet, F-35B Lightning II, and V-22 Osprey, the paper illustrates practical applications and solutions to these challenges. The significance of this research lies in its contribution to understanding the intricate aerodynamics of V/STOL aircraft, which is crucial for advancing their design and operational efficiency. By addressing the aerodynamic challenges and proposing potential solutions, this paper aims to support the continued development and innovation in V/STOL technology, ultimately enhancing its viability and performance in various aviation sectors.

Key Words

V/STOL ,Aerodynamics, Tiltrotor Aircraft, Tilting Aircraft , Vectored Thrust Aircraft , etc

Cite This Article

"Aerodynamics of V/STOL (Vertical/Short Takeoff and Landing) Aircraft", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.11, Issue 6, page no.b360-b373, June-2024, Available :http://www.jetir.org/papers/JETIR2406146.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

"Aerodynamics of V/STOL (Vertical/Short Takeoff and Landing) Aircraft", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.11, Issue 6, page no. ppb360-b373, June-2024, Available at : http://www.jetir.org/papers/JETIR2406146.pdf

Publication Details

Published Paper ID: JETIR2406146
Registration ID: 542358
Published In: Volume 11 | Issue 6 | Year June-2024
DOI (Digital Object Identifier):
Page No: b360-b373
Country: Meerut, Uttar Pradesh, India .
Area: Engineering
ISSN Number: 2349-5162
Publisher: IJ Publication


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