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Parameter optimization for an interactive aircraft design [PDF]
, 2011 The presentation introduces to aircraft preliminary design and optimization. Existing equations for the estimation of Specific Fuel Consumption, SFC are investigated. The Herrmann Model is selected for futher calculations. The aircraft design methodology
Niţă, Mihaela, Scholz, Dieter
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Analysis and Research on the Influence of Civil Aircraft System on CO2 Emission [PDF]
E3S Web of ConferencesBased on the international standard ICAO Annex 16 Volume III, this paper adopts the CO2 emission airworthiness calculation method proposed by ICAO to carry out sensitivity analysis and research on the influence of air intake volume of pneumatic system ...
Sun Kexin, Yang Yi, Xuan Zhaojie
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Science and Engineering of Composite Materials, 2021 This study experimentally investigates the effect of the opening configuration on the buckling stability and bearing performance of a structural beam web used in a commercial aircraft made of composite materials.
Sen Lin, Chenxi Li, Ying Hu, Hao Cong
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Review: key technologies for wide-body aircraft
Xibei Gongye Daxue XuebaoWide-body aircraft is the key technical product in the field of civil aviation. The development of wide-body aircraft is the important reflection of national comprehensive strength, as well as the inevitable course to achieve technological autonomy. This
ZHAO Chunling +5 more
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Continuous Open Access Special Issue "Aircraft Design": Number 2/2020
, 2020 Following the successful initial Special Issue on “Aircraft Design (SI-1/2017)”, this is already the second SI “Aircraft Design (SI-2/2020)”. Activities in the past showed that aircraft design may be a field too small to justify its own (subscription ...
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Civil Aircraft Design Priorities: Air Quality? Climate Change? Noise? [PDF]
, 2005 A variety of related questions is posed. Are the right priorities for future aircraft design being set now? New civil aircraft types could be ‘silent’, ie make much less noise than current types. They could be ‘green’, ie safeguard the environment.
Peter Brooker +2 more
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Computational Aerodynamics for Aircraft Design [PDF]
Science, 1989 This article outlines some of the principal issues in the development of numerical methods for the prediction of flows over aircraft and their use in the design process. These include the choice of an appropriate mathematical model, the design of shock-capturing algorithms, the treatment of complex geometric configurations, and shape modifications to ...
openaire +2 more sources
Aeroservoelastic analysis method for mixed-command fault of flight control system
Hangkong gongcheng jinzhanLarge civil aircraft fly-by-wire flight control systems may experience a fault condition where both normal mode and direct mode control commands are output simultaneously. It is necessary to propose a method to demonstrate the airworthiness compliance of
DING Luning, YANG Fei, LI Peng
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Performance Analysis of Abradable Coating Systems for Aircraft Gas Turbines
Advanced Engineering Materials, EarlyView.Three CoNiCrAlY/YSZ/MgAl2O4 abradable liner configurations on a nickel‐superalloy are evaluated by thermal‐gradient cycling and incursion tests. Laser ablation of the bondcoat and/or Y2O3‐stabilized ZrO2 (YSZ) intermediate layer increases mechanical interlocking and bonding for thick topcoats.
Hanna Heyl +4 more
wiley +1 more source
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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