$Aerodynamic performance of MAV wing with fuselage and stabilizer \ Muhammad Izzuddin Arif Abdul Samad$
QR Code

QR Code

Aerodynamic performance of MAV wing with fuselage and stabilizer \ Muhammad Izzuddin Arif Abdul Samad

The history of micro air vehicles (MAVs) really began with the development of model airplanes in the 19th century. However, the study of micro air vehicles (MAVs) is currently lack with the understanding of aerodynamics for the small aircraft flying at low speeds. Based on previous findings, the stu...

Full description

Bibliographic Details
Main Author:	Abdul Samad, Muhammad Izzuddin Arif
Format:	Student Project
Language:	English
Published:	2017
Subjects:	Aeronautics. Aeronautical engineering Mechanics of flight: Aerodynamics
Online Access:	https://ir.uitm.edu.my/id/eprint/35018/

Similar Items

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

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

Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
by: Mohd Ali, Zurriati
Published: (2015)

Aerodynamic performance of O-ring paper plane \ Amirul Ashraf Hassan
by: Hassan, Amirul Ashraf
Published: (2017)

Aerodynamics prediction of multi-purpose UAV using wind tunnel experimental approach / Ghazirah Mustapha @ Mustafa, Zurriati Mohd Ali, Wirachman Wisnoe
by: Mustapha @ Mustafa, Ghazirah, et al.
Published: (2009)

Interception loss canopy cover, C formulation theory / Azinoor Azida Abu Bakar … [et al.]
by: Abu Bakar, Azinoor Azida, et al.
Published: (2013)

Behaviour of symmetrical and asymmetrical geometries in fully immersed flow / Fauziah Jerai @ Junaidi
by: Jerai@Junaidi, Fauziah
Published: (2007)

Study of short period behaviour for BWB UAV / Mohd Safuan Rosli.
by: Rosli, Mohd Safuan
Published: (2009)

To study and simulate the concept of ramjet / Amiruddin Amkaromi
by: Amkaromi, Amiruddin
Published: (2005)

Aerodynamics of porous airfoils and wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2018)

Longitudinal Aerodynamic Characteristics of an Aircraft Model with and Without Winglet
by: Hossain, Md. Altab
Published: (2005)

A review on aerodynamics of nonflapping bird wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)

Investigation Of Aerodynamic Characteristics Of A Wing Model With Rgv Winglet
by: Gopal Krishnan, Sivaraj
Published: (2017)

Exploring potential benefits and challenges of touch screens on the flight deck
by: Avsar, Hüseyin
Published: (2017)

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 aerodynamic loading on thin substructure within transonic region of subsonic aircraft
by: Abdul Rahman, Umran
Published: (2018)

Educational software for stress analysis of an aircraft fuselage
by: Mohamed Ali, Jaafar Syed, et al.
Published: (2010)

Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device
by: Asrar, Waqar, et al.
Published: (2015)

Design of IIUM aircraft fuselage using composite material
by: Aminanda, Yulfian, et al.
Published: (2011)

Crash analysis of an aircraft fuselage under belly landing
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2017)

Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
by: Malik, Khurshid, et al.
Published: (2018)

CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
by: Munshi, Adnan, et al.
Published: (2018)

On the optimal model configuration for aerodynamic modeling of open cargo railway train
by: Golovanevskiy, Vladimir, et al.
Published: (2012)

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

Analysis of aerodynamic performance through flow simulation on x-plane with store-x
by: A.Rahman, Mahadhir
Published: (2019)

Aerodynamics investigation of delta wing at low Reynold’s number
by: Hamizi, Ilya Bashiera, et al.
Published: (2019)

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

Estimating vertical drag on helicopter fuselage during hovering
by: Wahab, A. A., et al.
Published: (2006)

Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris
by: Che Wan Idris, Che Wan Zaidie
Published: (2009)

Software development for aerodynamic characteristics estimation of wing-body combination of aircraft at cubsonic speeds
by: Dahalan, Md. Nizam, et al.
Published: (2001)

Effect of surface roughness on helicopter main rotor blade
by: Wan Rohizan, Wan Norhafizan
Published: (2017)

Vortex-induced vibration of a 5:1 rectangular cylinder: new computational and mathematical modelling approaches
by: Nguyen, Dinh Tung
Published: (2017)

Study of F1 car aerodynamics rear wing using computational fluid dynamic (CFD)
by: Mohd Shahmal, Mohd Shahid
Published: (2010)

Study of F1 car aerodynamics front wing using computational fluid dynamics (CFD)
by: Mohd Syazrul Shafiq, Saad
Published: (2010)

Effect of side wind on the directional stability and aerodynamics of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Longitudinal static stability of a blended wing-body unmanned aircraft with canard as longitudinal control surface / Rizal E. M. Nasir, Wahyu Kunjoro and Wirachman Wisnoe
by: E.M. Nasir, Rizal, et al.
Published: (2012)

Experimental investigation of the flow over IIUM-MAV using six component balance test and particle image velocimetry
by: Omar, Ashraf Ali, et al.
Published: (2011)

ESA 244 – AERODYNAMICS JANUARY 2014
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2014)

ESA 343 – AIRCRAFT AERODYNAMICS JANUARY 2014
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa
Published: (2014)

ESA 244/2 AERODYNAMICS (JUNE 2015)
by: PPKA, Pusat Pengajian Kejuruteraan Aeroangkasa