Development of the IIUM hybrid airship
Hybrid airship is an unconventional type of airship being developed since a few decades ago and is now being tried on a significant scale. In this paper, the preliminary design steps of a winged hull hybrid airship will be outlined and discussed together with a way to achieve controllability of the...
| Main Authors: | Ping, Julian T.K., Andan, Amelda D., Asrar, Waqar, Omar, Ashraf Ali |
|---|---|
| Format: | Proceeding Paper |
| Language: | English |
| Published: |
2010
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/2381/ http://irep.iium.edu.my/2381/1/paper_encon10.pdf |
Similar Items
Estimation of aerodynamic parameters of IIUM hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)
by: Andan, Amelda Dianne, et al.
Published: (2011)
Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012)
by: Andan, Amelda Dianne, et al.
Published: (2012)
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)
Aerodynamics of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)
by: Andan, Amelda Dianne, et al.
Published: (2011)
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)
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)
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)
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)
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)
Framework of conceptual design methodology for hybrid buoyant
aircraft
by: UlHaque, Anwar, et al.
Published: (2016)
by: UlHaque, Anwar, et al.
Published: (2016)
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)
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)
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)
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)
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)
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)
Span load modification via differential spoiler setting
by: Elsayed, Omer Ali, et al.
Published: (2010)
by: Elsayed, Omer Ali, et al.
Published: (2010)
Evaluation of aircraft wing-tip vortex using PIV
by: Elsayed, Omer Ali, et al.
Published: (2009)
by: Elsayed, Omer Ali, et al.
Published: (2009)
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)
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)
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)
Experimental investigation of free wing IIUM-UAV configuration
by: Omar, Ashraf Ali, et al.
Published: (2010)
by: Omar, Ashraf Ali, et al.
Published: (2010)
A high order compact-flowfield dependent variation (HOC-FDV)method for inviscid flows
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)
Higher order compact-flowfield dependent variation (HOCFDV)
method for solving navier-stokes equations
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)
Reynolds averaged navier-stokes flow computation of RAE2822 airfoil using gas-kinetic BGK Scheme
by: Ong, Jiunn Chit, et al.
Published: (2009)
by: Ong, Jiunn Chit, et al.
Published: (2009)
Numerical investigation of the vortical flow over delta wing and reverse delta wing
by: Omar, Ashraf Ali E., et al.
Published: (2012)
by: Omar, Ashraf Ali E., et al.
Published: (2012)
Similar Items
-
Estimation of aerodynamic parameters of IIUM hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011) -
Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012) -
Design and fabrication of a winged hybrid airship model for IIUM-LSWT
by: UlHaque, Anwar, et al.
Published: (2015) -
Aerodynamics of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011) -
Conceptual design of a winged hybrid airship
by: UlHaque, Anwar, et al.
Published: (2014)