Effect of canard to the aerodynamic characteristics of Blended Wing Body airplane

Ali, Zaileha Md; Kuntjoro, Wahyu; Wisnoe, Wirachman

doi:10.1109/isbeia.2012.6422979

Cited by 3 publications

(2 citation statements)

References 8 publications

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“…ZurriatiMohd Ali et al [17] developed an experiment to investigate the impact of canard angle on the aerodynamics of a blended wing body aircraft. The visualization of the air flow was enabled by using a physical mini bust model of a BWB aircraft when set at different angles of attack.…”

Section: Experimental Analysis Of Aircraft Fuselagementioning

confidence: 99%

Recent Developments of an Aircraft Fuselage along Theoretical, Experimental and Numerical Approach - A Review

Potty¹,

Angelo²,

Rao

et al. 2019

ujme

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Expressed in nature's infinite subtleties, the Fuselage draws its inspiration from the streamlined body of a bird or a fish, channelizing the flow of air around, enabling its ease in flight. Spanning most of the aircrafts structure, it plays a crucial role in the ferrying of people and cargo, simultaneously balancing the shears due to the empennage and wing structures all in mid-air. Its structural integrity is often questioned by failures due to load or bad air during maneuvers, causing instability which has led many to intensively explore and develop an ideal fuselage. The behaviour of the fuselage is crucially determined by the structural integrity and aerodynamic performance. This paper is an attempt at collating the recent technological advances pertaining to the fuselage. We've streamlined and categorised the wide-ranging scholarly articles by three fundamentally varying approaches-Theoretical, Experimental and Numerical. The theoretical approach saw the authors test out their hypothesis by utilizing and constructing various mathematical models using scientific principles with no verification by actual experimentation or simulation work. The experimental approach pertains to those papers whose authors devised experiments, whose data was used to draw distinct conclusions. The numerical approach mainly dealt with heavy computational analysis using FEM and CFD analysis. Therefore, this paper serves as a compendium for researchers and developers attempting to familiarise themselves with the current advancements and developments in domain of fuselage technology.

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Section: Experimental Analysis Of Aircraft Fuselagementioning

confidence: 99%

Recent Developments of an Aircraft Fuselage along Theoretical, Experimental and Numerical Approach - A Review

Potty¹,

Angelo²,

Rao

et al. 2019

ujme

View full text Add to dashboard Cite

show abstract

“…Although there has been some research on numeric analytical methods and finite element analysis (FEA), many methods on the design and optimization of the coil size, structure, and circuit structure cannot be verified experimentally due to the construction cost and site limitation of high-speed and full-size experimental prototypes. Usually, when the size of the research object is too large, the scaling models are often used for equivalent experiments [3] . In addition, in the field of electromagnetics, it is also a common means to excite the traveling wave magnetic field by coils with a special structure to simulate relative motion [4] .…”

Section: Introductionmentioning

confidence: 99%

Characteristic Analysis of the Equivalent Experimental System for Electrodynamic Suspension Linear Generator

Yu,

Wang,

Wang

et al. 2023

J. Phys.: Conf. Ser.

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This paper presents an equivalent experimental method for the linear generator of the electrodynamic suspension (EDS) system. Compared with the full-size experimental device, the proposed method can reduce the cost and difficulty of the experiment. Firstly, the working principle of the linear generator is described, and the numerical analytical expression for the induced voltage of the linear generator is derived. Based on the expression, the mapping relationship between the suspension coil current, system scaling ratio, and the induced voltage is clarified. Then, an equivalent experimental device was designed and built. Comparisons between the numeric analytical calculation, the finite element analysis, and the experiment have verified the accuracy of the equivalent experimental method.

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Experimental Studies of the Effect of Rectangular-Shaped Canard on a Generic Blended Wing Body (BWB)

Sanim,

Imisi-Oluwa,

Mat

et al. 2023

Lecture Notes in Mechanical Engineering

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Effect of canard to the aerodynamic characteristics of Blended Wing Body airplane

Cited by 3 publications

References 8 publications

Recent Developments of an Aircraft Fuselage along Theoretical, Experimental and Numerical Approach - A Review

Recent Developments of an Aircraft Fuselage along Theoretical, Experimental and Numerical Approach - A Review

Characteristic Analysis of the Equivalent Experimental System for Electrodynamic Suspension Linear Generator

Experimental Studies of the Effect of Rectangular-Shaped Canard on a Generic Blended Wing Body (BWB)

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