Investigation of aerodynamic parameters of a hybrid airship

QR Code

Investigation of aerodynamic parameters of a hybrid airship

The aerodynamic parameters of a preliminary winged-hull airship design are investigated. The research methodology involved the use of numerical simulation and wind tunnel testing. The aerodynamic parameters of the design are first computed using a commercial CFD code. The force and moment coefficien...

Full description

Bibliographic Details
Main Authors:	Andan, Amelda Dianne, Asrar, Waqar, Omar, Ashraf Ali
Format:	Article
Language:	English
Published:	American Institute of Aeronautical and Astronautic 2012
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/26573/ http://irep.iium.edu.my/26573/1/Investigation_of_Aerodynamic.pdf

Similar Items

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

Aerodynamics of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)

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

Conceptual design of a winged hybrid airship
by: UlHaque, Anwar, et al.
Published: (2014)

Static longitudinal stability of a hybrid airship
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)

Design and fabrication of a winged hybrid airship model for IIUM-LSWT
by: UlHaque, Anwar, et al.
Published: (2015)

Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach
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)

Aerodynamics of porous airfoils and wings
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)

Discrete tonal noise of NACA0015 airfoil at low reynolds number
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)

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)

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

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

Wind tunnel testing on a generic model of a hybrid lifting hull
by: UlHaque, Anwar, et al.
Published: (2016)

Numerical investigation of the flow over delta wing and reverse delta wing
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)

Numerical investigation of the vortical flow over delta wing and reverse delta wing
by: Omar, Ashraf Ali E., et al.
Published: (2012)

Yawing force of electric trimmers of a hybrid buoyant aerial vehicle
by: UlHaque, Anwar, et al.
Published: (2017)

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

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)

Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Half model testing for canard of a hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)

Wind tunnel testing of hybrid buoyant aerial vehicle
by: UlHaque, Anwar, et al.
Published: (2017)

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

Stability and takeoff ground roll issues of hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2014)

Assessment of engine's power budget for hydrogen powered hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Power-off static stability analysis of a clean configuration of a hybrid buoyant aircraft
by: Ul Haque, Anwar, et al.
Published: (2015)

Framework of conceptual design methodology for hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Hybrid buoyant aircraft: future STOL aircraft for interconnectivity of the Malaysian islands
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)

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

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

Numerical study of effect of spoiler configuration on wake vortex alleviation
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)

Study of the reverse delta wing
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)

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

Impact of a reverse delta type add-on device on the flap-tip vortex of a wing
by: Altaf, Afaq, et al.
Published: (2016)