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Development of an aircraft design expert system [PDF]
, 1988 The aircraft design process is characterised by the application of a wide range of knowledge across many disciplines based upon a certain degree of judgement and experience of the designer. A two pass approach has been taken towards the development of
Alsina, J.
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Conceptual design and optimization methodology for box wing aircraft [PDF]
, 2012 A conceptual design optimization methodology was developed for a medium range box wing aircraft. A baseline conventional cantilever wing aircraft designed for the same mis- sion and payload was also optimized alongside a baseline box wing aircraft.
Jemitola, Paul Olugbeji
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Research on operation scenario based aircraft power system architecture analysis and modelling [PDF]
E3S Web of Conferences, 2021 Aircraft power system is a complex system consisting of the power generation system, the power management and distribution system, and the power consumption system, which accounts for the aircraft's major fuel consumption and emissions.
Dongsheng Chen, Yan He, Mengqian Zhou
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Digital assembly process design for aircraft systems [PDF]
, 2012 The research described in this thesis concentrates on the development of an integrated assembly process design for aircraft systems. Assembly process design is one of the most important and complicated activities in aircraft manufacturing.
Li, Tao
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Exploring sub-strong scattering source of canopy of fighter with radar stealth technology
Xibei Gongye Daxue Xuebao, 2022 The canopy of a fighter is the main source of electromagnetic scattering, and the achievement of its radar stealth is one of key technologies for developing a stealth fighter.
ZHOU Tao +4 more
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Multi-objective aerodynamic optimization of flying-wing configuration based on adjoint method
Xibei Gongye Daxue Xuebao, 2021 In order to solve the multi-objective multi-constraint design in aerodynamic design of flying wing, the aerodynamic optimization design based on the adjoint method is studied. In terms of the principle of the adjoint equation, the boundary conditions and
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Civil Aircraft metal structure superfluous hole repair and stress evaluation method [PDF]
E3S Web of Conferences, 2021 Civil aircraft is the most complicated production of the world and during the manufacture various kinds of manufacture nonconformities occur at times. Superfluous hole is one of the most typical nonconformity types. When coping with this kind of problem,
Zhu Weibin +4 more
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Hangkong gongcheng jinzhan, 2021 The emergency door on the wing of a civil aircraft has particularity,and its fault is somewhat concealed,so it is particularly important to analyze its safety reasonably.The evaluation and selection principles of the latent failure of the emergency door ...
ZHU Zhengzheng +3 more
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Multi-disciplinary design of wings for transport aircraft operating at high subsonic speed [PDF]
, 1995 In this thesis a methodology for designing wings for transport aircraft operating at high subsonic speed is investigated. Several methods are studied, including more accurate methods such as the computational methods. These are used as an addition to
Djafri, Demil Y.
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Health Assessment Method for Military Aircraft Based on Mission Capabilities
Hangkong gongcheng jinzhan, 2020 The military aircraft health assessment has the problem of difficult application in engineering practice. The military aircraft is taken as the research object of health assessment, including task-oriented capability analysis, function analysis based on ...
FANG Guancheng +4 more
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