2019
DOI: 10.1016/j.cja.2019.05.018
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Effects of stability margin and thrust specific fuel consumption constrains on multi-disciplinary optimization for blended-wing-body design

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Cited by 14 publications
(7 citation statements)
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“…The manta ray biomimetic glider in the present paper is actually a Blended-Wing-Body (BWB) configuration, which is a revolutionary concept for commercial transports and a potential option for future civil aircraft and underwater glider (UG) [ 24 ]. Different from the traditional underwater vehicle, the BWB underwater glider merges the traditional fuselage and wing structure into a shape similar to a flying wing, which is able to glide through the water by controlling their buoyancy and converting the lift on wings into propulsive force without a power propulsion system [ 25 ].…”
Section: Resultsmentioning
confidence: 99%
“…The manta ray biomimetic glider in the present paper is actually a Blended-Wing-Body (BWB) configuration, which is a revolutionary concept for commercial transports and a potential option for future civil aircraft and underwater glider (UG) [ 24 ]. Different from the traditional underwater vehicle, the BWB underwater glider merges the traditional fuselage and wing structure into a shape similar to a flying wing, which is able to glide through the water by controlling their buoyancy and converting the lift on wings into propulsive force without a power propulsion system [ 25 ].…”
Section: Resultsmentioning
confidence: 99%
“…It is slightly lower for the BWB, which has good aerodynamic efficiency [27]. Therefore, the SWB aerodynamic design needs to be improved [28].…”
Section: Improvement Of Swb Aerodynamic Designmentioning
confidence: 99%
“…Firstly, this approach has been applied in research aimed at designing various aircraft configurations. The examples range from civil transport aircraft [30][31][32], conceptual BWB configurations [1,33,34] to other unconventional aircraft [35,36] and some unmanned airplanes [37,38]. Secondly, various achievements have been made in exploring the effects of this technique on the tradeoffs or benefits in terms of aircraft design [1,33,39].…”
Section: Introductionmentioning
confidence: 99%
“…The examples range from civil transport aircraft [30][31][32], conceptual BWB configurations [1,33,34] to other unconventional aircraft [35,36] and some unmanned airplanes [37,38]. Secondly, various achievements have been made in exploring the effects of this technique on the tradeoffs or benefits in terms of aircraft design [1,33,39]. For instance, the study in [1] presented that a higher L/D could be achieved by relaxing the static stability margin.…”
Section: Introductionmentioning
confidence: 99%
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