Conceptual design and simulation validation based finite element optimisation for tubercle leading edge composite wing of an unmanned aerial vehicle

QR Code

Conceptual design and simulation validation based finite element optimisation for tubercle leading edge composite wing of an unmanned aerial vehicle

A finite element model is developed to determine deformation and stresses on a composite wing of unmanned aerial vehicle (UAV) with a tubercle design at the leading edge of the wing. Tubercles, commonly known as protuberances found on the leading edge of a whale pectoral flipper, offering great perf...

Full description

Bibliographic Details
Main Authors:	Basri, Ernnie Illyani, Mustapha, Faizal, Hameed Sultan, Mohamed Thariq, Basri, Adi Azriff, Abas, Mohd Firdaus, Abdul Majid, Mohd Shukry, Ahmad, Kamarul Arifin
Format:	Article
Language:	English
Published:	Elsevier 2019
Online Access:	http://psasir.upm.edu.my/id/eprint/81007/ http://psasir.upm.edu.my/id/eprint/81007/1/FINITE.pdf

Similar Items

Numerical analysis of tubercles leading edge for unmanned aerial vehicle composite wing
by: Basri, Ernnie Illyani
Published: (2020)

Unmanned Aerial Vehicle (UAV) structural and manufacturing of conventional and humpback Tubercles Leading Edge (TLE) in aeronautical applications
by: Basri, Ernnie Illyani, et al.
Published: (2019)

Performance analysis of composite ply orientation in aeronautical application of unmanned aerial vehicle (UAV) NACA4415 wing
by: Basri, Ernnie Illyani, et al.
Published: (2019)

Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application
by: Basri, Ernnie Illyani, et al.
Published: (2021)

Performance analysis of composite laminates wing skin with the aid of fluid structure interaction of aerodynamic loading-structural analysis
by: Basri, Ernnie Illyani, et al.
Published: (2022)

UAV NACA4415 wing structural performance analysis subjected to external aerodynamic load using Schrenk’s approximation
by: Basri, Ernnie Illyani, et al.
Published: (2019)

Numerical and experimental study of leading edge tubercles with vortex generators on NACA 4415 airfoil
by: Aftab, Syed Mohammed Aminuddin
Published: (2017)

Numerical Simulation of the Effect of Leading-edge Tubercles on the Hydrodynamic Performance of Hydrofoils at Low and High Reynolds Numbers
by: Johnson, Peter
Published: (2018)

Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali, et al.
Published: (2010)

Aerodynamics effects of APC slow flyer propeller blade design with different airfoil origin positions
by: Ahmad Faris, Ahmad Fariduddin, et al.
Published: (2022)

Power sources for unmanned aerial vehicles: a state-of-the art
by: Saravanakumar, Yavinaash Naidu, et al.
Published: (2023)

Oscillating supersonic delta wings with curved leading edges
by: Khan, Sher Afghan, et al.
Published: (2010)

Oscillating supersonic delta wing with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)

Oscillating supersonic delta wings with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)

Design, fabrication and experimental testing of IIUM free wing unmanned aerial vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali E., et al.
Published: (2011)

Development of a Fixed Wing Unmanned Aerial Vehicle (UAV) for Disaster Area Monitoring and Mapping
by: Gesang, Nugroho, et al.
Published: (2015)

Design And Development Of A Fixed-Wing Vertical Take-Off And Landing Unmanned Aerial Vehicle
by: Wong, Seng Man
Published: (2018)

Computation fluid dynamics study on aerodynamics blade design of Advance Precision Composite (APC) slow flyer propeller
by: Ahmad Faris, Ahmad Fariduddin, et al.
Published: (2020)

Unmanned aerial vehicle platform
by: Khalid, Khateeb
Published: (2010)

Review on type of sensors and detection method of anti-collision system of unmanned aerial vehicle
by: Chandran, Navaneetha Krishna, et al.
Published: (2023)

Aerial and underwater sound of unmanned aerial vehicles (UAV)
by: Erbe, Christine, et al.
Published: (2017)

Conceptual design of flapping wing using shape memory alloy actuator for micro unmanned aerial vehicle
by: Marimuthu, Navanitha, et al.
Published: (2014)

Study on the effects of individual pitot tube inlet of a bladeless Tesla microturbine using numerical analysis
by: Basri, Ernnie Illyani, et al.
Published: (2023)

Mathematical Modelling of an Unmanned Aerial Vehicle
by: Chong, Chiew Choy
Published: (2005)

Computation of stiffness derivative for an unsteady delta wing with curved leading edges
by: Monis, Renita Sharon, et al.
Published: (2017)

Optimization of a blended-wing-body unmanned aerial vehicle design for maximum aerodynamic lift-to-drag ratio
by: Romli, Fairuz Izzuddin, et al.
Published: (2023)

Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012)

Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
by: Crasta, Asha, et al.
Published: (2013)

Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge
by: Renita, sharon Monis, et al.
Published: (2019)

Development and control of Unmanned Aerial Vehicle (UAV)
by: Sidek, Shahrul Na'im, et al.
Published: (2011)

Design of an autopilot for an autonomous unmanned aerial vehicle
by: Idres, Moumen, et al.
Published: (2011)

Development of unmanned aerial vehicle – Part 1
by: Sidek, Shahrul Na'im, et al.
Published: (2011)

Development of unmanned aerial vehicle – Part 2
by: Sidek, Shahrul Na'im, et al.
Published: (2011)

Affordable unmanned aerial vehicle aircraft for surveillance
by: Sidek, Shahrul Na'im, et al.
Published: (2010)

Unmanned aerial vehicle quadcopter: a review
by: Bashi, Omar Ibrahim Dallal, et al.
Published: (2017)

Unmanned aerial vehicle quadcopter: a review
by: Bashi, Omar I. Dallal, et al.
Published: (2017)

Obstacle detection for Unmanned Aerial Vehicle (UAV)
by: Abdul Khaliq, Nor Aizatul Nabila, et al.
Published: (2022)

Review on dislodgement & securement risk of peripheral intravenous Catheter/Cannula and the needs of PIVC securement device
by: Zainul Fadziruddin, Zubair Faramir, et al.
Published: (2020)

Design for modularity of Blended Wing Body (BWB) baseline ii-E2 Unmanned Aerial Vehicle (UAV) / Matzaini Katon
by: Katon, Matzaini
Published: (2014)

Evaluation of stiffness derivative for a delta wing with straight leading edges in unsteady flow
by: Renita, Sharon Monis, et al.
Published: (2019)