Authors :
Ashwin Wankhede; Akshat Joshi; Pratham Kale; Harshvardhan Sandbhor; Krishna. B. Jadhav
Volume/Issue :
Volume 9 - 2024, Issue 2 - February
Google Scholar :
https://tinyurl.com/bdeht38a
Scribd :
https://tinyurl.com/3p8rhfhe
DOI :
https://doi.org/10.38124/ijisrt/IJISRT24FEB447
Abstract :
This project report details the original
conceptualization, design, and analysis of a morphing
wing structure for fixed-wing Unmanned Aerial Vehicles
(UAVs). Our approach incorporates an octahedron cell
structure coupled with the application of shape memory
alloys(SMAs) to facilitate controlled wing morphing. The
primary goal is to augment the UAVs aerodynamic
efficiency and adaptability to various flight conditions.
The octahedron cell structure is employed as the
foundational framework, providing a balance between
structural integrity andflexibility for shape adjustments.
The integration of shape memory alloys, known for their
reversible phase transformations, enables precise and
efficient control over the morphing process. Through
this combination, we aim to optimize the UAVs flight
characteristics, including improved efficiency, stability,
and maneuver ability.
To validate the feasibility and performance of the
morphing wing design, Finite Element Analysis (FEA)
has been conducted. This computational approach
allows for a comprehensive evaluation of the structural
integrity and aerodynamic behavior of the morphing
wing under diverse loading conditions. The FEAresults
offer crucial insights into the structural response, stress
distribution, and deformation patterns, guiding the
iterative refinement of the design for optimal
functionality.
This project represents a unique contribution to
UAV technology, presenting an original perspective on
morphing wing design that harnesses the benefits of
octahedron cell structureand shape memory alloys. The
insights gained from the FEA analysis provide valuable
guidance for the ongoing development and
implementation of morphing wing structures in fixed-
wing UAVs. This work sets the stage for improved
adaptability and performance in a range of operational
scenarios, without reliance on external sources or
existing research
This project report details the original
conceptualization, design, and analysis of a morphing
wing structure for fixed-wing Unmanned Aerial Vehicles
(UAVs). Our approach incorporates an octahedron cell
structure coupled with the application of shape memory
alloys(SMAs) to facilitate controlled wing morphing. The
primary goal is to augment the UAVs aerodynamic
efficiency and adaptability to various flight conditions.
The octahedron cell structure is employed as the
foundational framework, providing a balance between
structural integrity andflexibility for shape adjustments.
The integration of shape memory alloys, known for their
reversible phase transformations, enables precise and
efficient control over the morphing process. Through
this combination, we aim to optimize the UAVs flight
characteristics, including improved efficiency, stability,
and maneuver ability.
To validate the feasibility and performance of the
morphing wing design, Finite Element Analysis (FEA)
has been conducted. This computational approach
allows for a comprehensive evaluation of the structural
integrity and aerodynamic behavior of the morphing
wing under diverse loading conditions. The FEAresults
offer crucial insights into the structural response, stress
distribution, and deformation patterns, guiding the
iterative refinement of the design for optimal
functionality.
This project represents a unique contribution to
UAV technology, presenting an original perspective on
morphing wing design that harnesses the benefits of
octahedron cell structureand shape memory alloys. The
insights gained from the FEA analysis provide valuable
guidance for the ongoing development and
implementation of morphing wing structures in fixed-
wing UAVs. This work sets the stage for improved
adaptability and performance in a range of operational
scenarios, without reliance on external sources or
existing research
