IIUM Geobat flying saucer: design, fabrication and testing

IIUM Geobat flying saucer: design, fabrication and testing

In this work, the first IIUM circular planform unmanned Aerial vehicle (IIUM-CPUAV), also known as Geobat flying saucer, was successfully designed, built and tested by the team from the Department of Mechanical Engineering, IIUM. The designing process started with gathering historical data and perfo...

Descrizione completa

Dettagli Bibliografici
Autore principale:	Omar, Ashraf Ali E.
Natura:	Monograph
Lingua:	English
Pubblicazione:	s.n. 2012
Soggetti:	TL500 Aeronautics
Accesso online:	http://irep.iium.edu.my/33516/1/EDW_A11-056.pdf

Documenti analoghi

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

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

Development of the IIUM hybrid airship
di: Ping, Julian T.K., et al.
Pubblicazione: (2010)

Estimation of aerodynamic parameters of IIUM hybrid airship
di: Andan, Amelda Dianne, et al.
Pubblicazione: (2011)

Experimental investigation of free wing IIUM-UAV configuration
di: Omar, Ashraf Ali, et al.
Pubblicazione: (2010)

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

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

Design and development of IIUM hovercraft
di: Syed Mohamed Ali, Jaffar, et al.
Pubblicazione: (2013)

Study of the reverse delta wing
di: Altaf, Afaq, et al.
Pubblicazione: (2011)

Experimental investigation of the vortical flow around a reverse delta wing using PIV
di: Altaf, Afaq, et al.
Pubblicazione: (2010)

Span load modification via differential spoiler setting
di: Elsayed, Omer Ali, et al.
Pubblicazione: (2010)

Evaluation of aircraft wing-tip vortex using PIV
di: Elsayed, Omer Ali, et al.
Pubblicazione: (2009)

A high order compact-flowfield dependent variation (HOC-FDV)method for inviscid flows
di: Elfaghi, Abdulhafid M., et al.
Pubblicazione: (2010)

Higher order compact-flowfield dependent variation (HOCFDV) method for solving navier-stokes equations
di: Elfaghi, Abdulhafid M., et al.
Pubblicazione: (2010)

Reynolds averaged navier-stokes flow computation of RAE2822 airfoil using gas-kinetic BGK Scheme
di: Ong, Jiunn Chit, et al.
Pubblicazione: (2009)

Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)
di: Elsayed, Omer Ali, et al.
Pubblicazione: (2011)

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

Higher order compact-flowfield dependent variation (HOC-FDV) solution of one-dimensional problems
di: Elfaghi, Abdulhafid M., et al.
Pubblicazione: (2010)

The accuracy of the gas-kinetic BGK finite difference method for solving 3-D compressible inviscid flows
di: Ong, Jiunn Chit, et al.
Pubblicazione: (2011)

Evolution of NACA23012 wake vortices structure using PIV
di: Elsayed, Omer Ali, et al.
Pubblicazione: (2012)

Influence of differential spoiler settings on the wake the vortex characterization and alleviation
di: Elsayed, Omer Ali, et al.
Pubblicazione: (2010)

Inﬂuence of differential spoiler settings on the wake vortex characterization and alleviation
di: Elsayed, Omer Ali, et al.
Pubblicazione: (2010)

Flow visualization over a circular planform wing
di: Suliman , M. M. Ali, et al.
Pubblicazione: (2013)

Investigation of the vortical flow around a reverse delta wing
di: Altaf, Afaq, et al.
Pubblicazione: (2011)

Highly accurate compact flowfield dependent variation method for solving two-dimensional navier-stokes equations
di: Elfagi, Abdulhafid M., et al.
Pubblicazione: (2011)

Experimental investigation of wing tip vortex
di: Elsayed, Omer Ali, et al.
Pubblicazione: (2009)

Hypersonic flow simulation by the gas-kinetic bhatnagar-gross-krook scheme
di: Chit, O.J., et al.
Pubblicazione: (2005)

The Efficiency of Gas-Kinetic BGK scheme for solving 2-d compressible inviscid regular shock reflection problem
di: Ong, Jiunn Chit, et al.
Pubblicazione: (2004)

A gas-kinetic BGK solver for two-dimensional turbulent compressible flow
di: Ong, Jiunn Chit, et al.
Pubblicazione: (2008)

Numerical simulation of a low aspect ratio wing at low Reynolds number
di: Suliman , M. M. Ali, et al.
Pubblicazione: (2013)

Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
di: Mawlood, M.K., et al.
Pubblicazione: (2006)

Application of Gas-Kinetic BGK Scheme for Solving 2-D Compressible Inviscid Flow around Linear Turbine Cascade
di: Abdusslam, Saleh N., et al.
Pubblicazione: (2006)

Aerodynamics of airfoil sections and their influence on wind turbine design and performance
di: Abdelrahman, Mohammad, et al.
Pubblicazione: (2011)

Educational software for stress analysis of thin-walled sections 1 : Isotropic material
di: Ismail, Nurhuda, et al.
Pubblicazione: (2011)

Educational software for stress analysis of thin-walled sections 2: Composite material
di: Mohamed Ali, Jaafar Syed, et al.
Pubblicazione: (2011)

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

Design, Fabrication of IIUM Unmanned Air Vehicle
di: Omar, Ashraf A., et al.
Pubblicazione: (2006)

On the evaluation of negative altitude requirement for flutter speed boundary of transport aircraft and UAV
di: Sulaeman, Erwin
Pubblicazione: (2012)

Flutter analysis of supersonic wing with external stores
di: Abdullah, Nur Azam, et al.
Pubblicazione: (2013)

Alternate approximate function for kernel function of oscillating lifting surfaces
di: Sulaeman, Erwin, et al.
Pubblicazione: (2013)