Estimation of aerodynamic parameters of IIUM hybrid airship
The aerodynamic parameters of a preliminary IIUM low speed winged-hull airship design is investigated. The objective is to study the aerodynamic parameters of the wingedhull airship and to find the necessities of attaching wings to the existing IIUM low speed airship. The research methodology invo...
| Main Authors: | Andan, Amelda Dianne, Asrar, Waqar, Omar, Ashraf Ali |
|---|---|
| Format: | Proceeding Paper |
| Language: | English |
| Published: |
2011
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/2344/ http://irep.iium.edu.my/2344/1/ICMAE-paper_1.pdf |
Similar Items
Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012)
by: Andan, Amelda Dianne, et al.
Published: (2012)
Development of the IIUM hybrid airship
by: Ping, Julian T.K., et al.
Published: (2010)
by: Ping, Julian T.K., et al.
Published: (2010)
Aerodynamics of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)
by: Andan, Amelda Dianne, et al.
Published: (2011)
Design and fabrication of a winged hybrid airship model for IIUM-LSWT
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Conceptual design of a winged hybrid airship
by: UlHaque, Anwar, et al.
Published: (2014)
by: UlHaque, Anwar, et al.
Published: (2014)
Static longitudinal stability of a hybrid airship
by: ul-Haque, Anwar, et al.
Published: (2014)
by: ul-Haque, Anwar, et al.
Published: (2014)
Comparison of digital DATCOM and wind tunnel data of a winged hybrid airship’s generic model
by: Ul Haque, Anwar, et al.
Published: (2014)
by: Ul Haque, Anwar, et al.
Published: (2014)
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Effect of side wind on the directional stability and aerodynamics of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
Aerodynamics of porous airfoils and wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2018)
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2018)
A review on aerodynamics of nonflapping bird wings
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2016)
Discrete tonal noise of NACA0015 airfoil at low reynolds
number
by: Andan, Amelda Dianne, et al.
Published: (2019)
by: Andan, Amelda Dianne, et al.
Published: (2019)
Effect of external acoustic excitation on NACA0015 discrete tonal noise
by: Andan, Amelda Dianne, et al.
Published: (2018)
by: Andan, Amelda Dianne, et al.
Published: (2018)
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)
by: Asrar, Waqar, et al.
Published: (2015)
Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
by: Malik, Khurshid, et al.
Published: (2018)
by: Malik, Khurshid, et al.
Published: (2018)
Wind tunnel testing on a generic model of a hybrid lifting hull
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
Wind tunnel testing of hybrid buoyant aerial vehicle
by: UlHaque, Anwar, et al.
Published: (2017)
by: UlHaque, Anwar, et al.
Published: (2017)
Stability and takeoff ground roll issues of hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2014)
by: UlHaque, Anwar, et al.
Published: (2014)
Design, fabrication and experimental testing of IIUM free wing unmanned aerial vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali E., et al.
Published: (2011)
by: Omar, Ashraf Ali E., et al.
Published: (2011)
Yawing force of electric trimmers of a hybrid buoyant aerial vehicle
by: UlHaque, Anwar, et al.
Published: (2017)
by: UlHaque, Anwar, et al.
Published: (2017)
Assessment of engine's power budget for hydrogen
powered hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
Development of IIUM Free Wing Unmanned Aerial Vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali, et al.
Published: (2010)
by: Omar, Ashraf Ali, et al.
Published: (2010)
Framework of conceptual design methodology for hybrid buoyant
aircraft
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
Development of IIUM circular planform unmanned aerial
vehicle (IIUM-CPUAV)
by: Omar, Ashraf Ali, et al.
Published: (2012)
by: Omar, Ashraf Ali, et al.
Published: (2012)
Half model testing for canard of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
IIUM Geobat flying saucer: design, fabrication and testing
by: Omar, Ashraf Ali E.
Published: (2012)
by: Omar, Ashraf Ali E.
Published: (2012)
Hybrid buoyant aircraft: future STOL aircraft for interconnectivity of the Malaysian islands
by: UlHaque, Anwar, et al.
Published: (2017)
by: UlHaque, Anwar, et al.
Published: (2017)
Establishing the analytical relationships for mass and volumetric mass fractions for hybrid boyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)
by: UlHaque, Anwar, et al.
Published: (2015)
Power-off static stability analysis of a clean configuration of a hybrid buoyant aircraft
by: Ul Haque, Anwar, et al.
Published: (2015)
by: Ul Haque, Anwar, et al.
Published: (2015)
Evaluation of aircraft wing-tip vortex using PIV
by: Elsayed, Omer Ali, et al.
Published: (2009)
by: Elsayed, Omer Ali, et al.
Published: (2009)
Span load modification via differential spoiler setting
by: Elsayed, Omer Ali, et al.
Published: (2010)
by: Elsayed, Omer Ali, et al.
Published: (2010)
Study of the reverse delta wing
by: Altaf, Afaq, et al.
Published: (2011)
by: Altaf, Afaq, et al.
Published: (2011)
The accuracy of the gas-kinetic BGK finite difference
method for solving 3-D compressible inviscid flows
by: Ong, Jiunn Chit, et al.
Published: (2011)
by: Ong, Jiunn Chit, et al.
Published: (2011)
Numerical investigation of the flow over delta wing and reverse delta wing
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
Numerical study of effect of spoiler configuration on
wake vortex alleviation
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)
Higher order compact-flowfield dependent variation (HOC-FDV) solution of one-dimensional problems
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)
Experimental investigation of the vortical flow around a reverse delta wing using PIV
by: Altaf, Afaq, et al.
Published: (2010)
by: Altaf, Afaq, et al.
Published: (2010)
Development of International Islamic University Malaysia-Micro Aerial Vehicle (IIUM-MAV)
by: Omar, Ashraf Ali, et al.
Published: (2009)
by: Omar, Ashraf Ali, et al.
Published: (2009)
Experimental investigation of free wing IIUM-UAV configuration
by: Omar, Ashraf Ali, et al.
Published: (2010)
by: Omar, Ashraf Ali, et al.
Published: (2010)
Similar Items
-
Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012) -
Development of the IIUM hybrid airship
by: Ping, Julian T.K., et al.
Published: (2010) -
Aerodynamics of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011) -
Design and fabrication of a winged hybrid airship model for IIUM-LSWT
by: UlHaque, Anwar, et al.
Published: (2015) -
Conceptual design of a winged hybrid airship
by: UlHaque, Anwar, et al.
Published: (2014)