Half model testing for canard of a hybrid buoyant aircraft

QR Code

Half model testing for canard of a hybrid buoyant aircraft

Due to the interference effects, the intrinsic aerodynamic parameters obtained from the individual component testing are always fundamentally different than those obtained for complete model testing. Consideration and limitation for such testing need to be taken into account in any design work r...

Full description

Bibliographic Details
Main Authors:	UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin, Syed Mohamed Ali, Jaffar
Format:	Article
Language:	English
Published:	World Academy of Science, Engineering and Technology 2015
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/46474/ http://irep.iium.edu.my/46474/1/Half-Model-Testing-for-Canard-of-a-Hybrid-Buoyant-Aircraft.pdf

Similar Items

Hybrid buoyant aircraft: future STOL aircraft for interconnectivity of the Malaysian islands
by: UlHaque, Anwar, et al.
Published: (2017)

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

Establishing the analytical relationships for mass and volumetric mass fractions for hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2016)

Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach
by: UlHaque, Anwar, et al.
Published: (2015)

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)

Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft
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)

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

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

Yawing force of electric trimmers of a hybrid buoyant aerial vehicle
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)

Hydrostatic and hydrodynamic characteristics of swimming animals: an inspiration for hybrid buoyant aircraft
by: UlHaque, Anwar, et al.
Published: (2015)

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

Effect of diamond shaped strut with cylindrical pitch rod in subsonic wind tunnel testing
by: UlHaque, Anwar, et al.
Published: (2017)

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

Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed
by: UlHaque, Anwar, et al.
Published: (2015)

Static longitudinal stability of a hybrid airship
by: ul-Haque, Anwar, et al.
Published: (2014)

Literature review : Biomimetic and conventional aircraft wing tips
by: Ahmed Siddiqui, Naseeb, et al.
Published: (2017)

A novel technique to neutralize the Yawing moment due to asymmetric thrust in a hybrid buoyant aircraft
by: Haque, Anwar Ul, et al.
Published: (2016)

Cambered profile of a California sea lion's body
by: UlHaque, Anwar, et al.
Published: (2015)

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)

Defining reference area for prediction of aerodynamic coefficients of a biologically inspired hybrid buoyant vehicle
by: Haque, Anwar Ul, et al.
Published: (2017)

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

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

A prospective solution For consistent aerostatic lift for a hybrid buoyant aircraft
by: Haque, Anwar Ul, et al.
Published: (2016)

Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
by: Malik, Khurshid, 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)

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

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

Structural design of hybrid buoyant aircraft's model for subsonic wind tunnel testing
by: , Anwar-Ul-Haque, et al.
Published: (2017)

Effect of a directionally porous wing tip on tip vortex
by: Mohammed Aldheeb, Mohammed Abdulmalek, et al.
Published: (2020)

Experimental investigation of a new spiral wingtip
by: Siddiqui, Naseeb, et al.
Published: (2018)

Experimental and numerical study on the aerodynamics and stability characteristics of a canard aircraft
by: Syed Mohamed Ali, Jaffar, et al.
Published: (2019)

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

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)

Comparison of data correction methods for blockage effects in semispan wing model testing
by: UlHaque, Anwar, et al.
Published: (2016)

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