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Optimal design of a flying-wing aircraft inner wing structure configuration [PDF]
, 2012 Flying-wing aircraft are considered to have great advantages and potentials in aerodynamic performance and weight saving. However, they also have many challenges in design.
Huang, Haidong
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Preliminary fuselage structural configuration of a flying-wing type airline [PDF]
, 2012 The flying-wing is a type of configuration which is a tailless airplane accommodating all of its parts within the outline of a single airfoil. Theoretically, it has the most aerodynamic efficiency.
Cheng, Yun
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High Speed Marine Vehicles With Aerodynamic Surfaces: Development of a Dynamic Model for a Novel Configuration. [PDF]
, 2008 A research programme on high speed marine vehicles fitted with aerodynamic surfaces started in Cranfield University in 2005. One of the configurations analyzed is a high speed prismatic planing hull with one or more aerodynamic surfaces; it is called ...
Patel, Minoo H. +2 more
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Hangkong gongcheng jinzhan, 2020 The accelerating effect, viscous effect, and rotating effect of the propeller slipstream are of significant influences on the performance of the inlet.
WANG Limin, ZHANG Yanjun
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Mathematical and Computer Modelling of Dynamical Systems, 2023 The influence of the powered effect on the aerodynamic performance of the blended-wing-body (BWB) takeoff configuration is analysed in this study by solving the three-dimensional Reynolds-averaged Navier–Stokes equation on a multiblock structured grid ...
Gang Yu, Dong Li, Yuling Duan
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Aerodynamic Characterization of Hypersonic Transportation Systems and Its Impact on Mission Analysis
Energies, 2021 This paper aims to provide technical insights on the aerodynamic characterization activities performed in the field of the H2020 STRATOFLY project, for the Mach 8 waverider reference configuration.
Nicole Viola +3 more
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The comparison of aerodynamic and stability characteristics between conventional and blended wing body aircraft [PDF]
, 2012 Aircraft with advanced wing geometry, like the flying wing or blended wing body configuration, seems to be the seed candidate of future aircraft. Compared with conventional aircraft, there are significant aerodynamic performance improvements because of ...
Wang, Faliang
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Drag Characteristics and Reduction Test for Hub of Coaxial-rotor Helicopter
Hangkong gongcheng jinzhan, 2020 The drag of coaxial helicopter hub accounts is more than 50% of the total helicopter's waste drag, so it is necessary to research the drag characteristics and reduction design of the hub. Wind tunnel test is carried out for a coaxial helicopter hub model,
LONG Haibin, WU Yuping
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Applied Sciences, 2021 This paper puts forward an aerodynamic design method to improve the high-speed aerodynamic performance of an aircraft with low-aspect-ratio tailless configuration.
Zhongyuan Liu, Lie Luo, Binqian Zhang
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Study on Aircraft Reliability Assessment in Flight Test and Service Period
Hangkong gongcheng jinzhan, 2020 The reliability level is one of the most significant indexes to be considered in aircraft design process. In order to guarantee the objectivity and accuracy of results, the study on aircraft reliability assessment in flight test and service period is ...
GUO Peng, ZHAO Xiaodong
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