Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)

QR Code

Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)

Micro Aerial Vehicle (MAV) in Malaysia is still at an early stage. Therefore, the development of flapping a wing MAV by Aerodynamic Laboratory in School of Mechanical Universiti Sains Malaysia, encourage the local researchers and scientist to study the importance and the capability of flapping a win...

Full description

Bibliographic Details
Main Author:	Rashid, Rohayati Ab
Format:	Thesis
Language:	English
Published:	2011
Subjects:	TJ1 Mechanical engineering and machinery
Online Access:	http://eprints.usm.my/42449/ http://eprints.usm.my/42449/1/ROHAYATI_AB_RASHID.pdf

Similar Items

Experimental And Numerical Investigations On The Performance Of Flexible Skin Flapping Wing For Micro Aerial Vehicle Application
by: Yusoff, Hamid
Published: (2013)

Experimental Study on the Effect of Skin Flexibility on Aerodynamic Performance of Flapping Wings for Micro Air Vehicles
by: Hamid, Yusoff, et al.
Published: (2014)

Experimental investigation of plain- and flapped-wing tip vortices
by: Elsayed, Omer Ali, et al.
Published: (2009)

Kinematic and aerodynamic modelling of bi- and quad-wing flapping wing micro-air-vehicle
by: Djojodihardjo, Harijono, et al.
Published: (2016)

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

Linear model identification of beetle-mimicking flapping wing micro-air vehicle in hovering flight
by: Khan, Qudrat, et al.
Published: (2016)

Adaptive control strategies for button motor actuated insect scale flapping wing MAV mechanisms
by: Singh, Spoorthi, et al.
Published: (2025)

Aerodynamics performance of optimal wing profile on MAV wings / Siti Khatijah Hamdan
by: Hamdan, Siti Khatijah

Experimental aerodynamics of washout twist morphing MAV wing / Muhammad Hakim Mohd Hafiz
by: Mohd Hafiz, Muhammad Hakim
Published: (2017)

Design of flapping mechanism and analysis on the lift force of the wings / Saktishvikmend Anbalagan
by: Saktishvikmend, Anbalagan
Published: (2019)

Effect of wing deformation on the aerodynamic performance of flapping wings: fluid-structure interaction approach
by: Fairuz, Z. M., et al.
Published: (2016)

Effects of flapping wing micro air vehicle's pitching angle on stability at low reynolds number
by: Mowhoub, Mohamed, et al.
Published: (2023)

Temperature feedback control of coated shape memory alloy for micro air vehicle flapping wing
by: Awang Jumat, Nurkhairunisa
Published: (2020)

Gust load alleviation of flexible composite wing
by: Ibren, Mohamed, et al.
Published: (2020)

Analysis of one way valve mechanism for wings of a flapping drone / Deng Xinchen
by: Deng, Xinchen
Published: (2020)

Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
by: Omar, Ashraf Ali, et al.
Published: (2009)

Numerical investigation of Kingfisher’s wing under multi-phase flight for micro-aerial-vehicle
by: Abas, Mohd Firdaus
Published: (2019)

Development of an optimal dragonfly-like flapping wing structure for use in biomimetic micro air vehicles / Praveena Nair Sivasankaran
by: Praveena Nair, Sivasankaran
Published: (2016)

Shape optimisation and performance analysis of flapping wings
by: Ghommem, M., et al.
Published: (2012)

On the shape optimization of flapping wings and their performance analysis
by: Ghommem, M., et al.
Published: (2014)

Kinematic and aerodynamic modelling of flapping wing ornithopter.
by: Djojodihardjoa, Harijono, et al.
Published: (2012)

Aerodynamic performances of twist morphing MAV wing / Noor Iswadi Ismail
by: Ismail, Noor Iswadi
Published: (2015)

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

Flapping wing mechanism development and control / Nurasyeera Rohaizat
by: Nurasyeera , Rohaizat
Published: (2018)

Mathematical modelling of aerodynamic characteristics for flapping wing ornithopter
by: Ramli, Alif Syamim Syazwan
Published: (2015)

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

An Experimental Study Of Oscillating Subboundary Layer Vortex Generators Application On A Wing'S Flap
by: Hussin, Fauzi
Published: (2014)

Modelling and structural analysis of three-dimensional wing
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)

Identification of Nonlinearities in Joints of a Wing Structure
by: M. S. M., Sani, et al.
Published: (2016)

Aerodynamic performance of MAV wing with fuselage and stabilizer \ Muhammad Izzuddin Arif Abdul Samad
by: Abdul Samad, Muhammad Izzuddin Arif
Published: (2017)

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

Flapping wings in line formation flight: A computational analysis
by: Ghommem, M., et al.
Published: (2014)

Induced rolling moment for NACA4412 plain and flapped wing
by: Elsayed, Omer Ali, et al.
Published: (2010)

Structural dynamic characterization of biobased micro aerial vehicles / Rubentheren Viyapuri
by: Rubentheren, Viyapuri
Published: (2013)

Flapping membrane wing: a prediction towards inter-domain flight
by: Abas, M. F., et al.
Published: (2016)

Vortex Lattice Simulations of Attached and Separated Flows around Flapping Wings
by: Thomas, Lambert, et al.
Published: (2017)

The analysis of wing performance for reconnaissance UAV
by: Zulkifli, Yusof
Published: (2009)

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)

Experimental investigation of the influence of a reverse delta type add-on device on the flap-tip vortex of a wing
by: Altaf, Afaq, et al.
Published: (2017)