High-lift design methodology for subsonic civil transport aircraft

Dam, C. P. van; Paris, J. K.; Kam, Jeremy C. Vander

doi:10.1109/aero.2000.878216

Cited by 2 publications

(2 citation statements)

References 13 publications

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“…Promising results have been obtained from this type of study (Kusunose and Cao, 1994). This extension of the methodology will provide greater confidence in the solutions developed by INS2D, and is described in more detail in an upcoming paper (van Dam et al, 1999).…”

Section: Contributed Papermentioning

confidence: 87%

Aero‐mechanical design of high‐lift systems

Dam

Shaw

Kam

et al. 1999

Aircraft Engineering and Aerospace Technology

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In today’s highly competitive and economically driven commercial aviation market, the trend is to make aircraft systems simpler and to design and develop them faster resulting in lower production and operational costs. One such system is the high‐lift system. A methodology has been developed which merges aerodynamic data with kinematic analysis of the trailing‐edge flap mechanism with minimum mechanism definition required. This methodology provides quick and accurate aerodynamic performance prediction of the flap deployment mechanism early on in the high‐lift system preliminary design stage. Sample analysis results for four different deployment mechanisms are presented as well as descriptions of the aerodynamic and mechanism data required for evaluation. Extensions to interactive design capabilities are also discussed.

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Section: Contributed Papermentioning

confidence: 87%

Aero‐mechanical design of high‐lift systems

Dam

Shaw

Kam

et al. 1999

Aircraft Engineering and Aerospace Technology

Self Cite

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“…The high-lift system is one important part of modern large transport aircraft, which composes of flaps, a support truss, a drive mechanism, and control systems etc. The system is important for aircraft performance in both takeoff and landing [1]. The objectives for development of the high-lift system are to achieve the three objectives i.e.…”

Section: Introductionmentioning

confidence: 99%

High-Lift Mechanism Motion Generation Synthesis Using a Metaheuristic

Chabphet

Santichatsak

Thalang

et al. 2019

Innovation Aviation &Amp;amp; Aerospace Industry - International Conference 2020

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This paper proposes an approach to synthesize a high-lift mechanism (HLM) of a transportation aircraft. Such a mechanism is very important for generation of additional lift to an aircraft wing during take-off and landing. The design problem is minimization of error between the motions of a four-bar mechanism for controlling a flap to the target points. The optimum target points are positions and angles of flap at the take-off and landing conditions, which are designed based on maximizing the lift to drag ratio. Design constraints include the conditions of four-bar mechanism to work properly, limiting positions and workplace of the mechanism. A optimizer used in this study, is in a group of metaheuristics (MHs). The results show the optimum mechanism can generate flap motion fulfilling the design targets, thus, the proposed technique can be used to increase the performance of HLM.

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High-lift design methodology for subsonic civil transport aircraft

Cited by 2 publications

References 13 publications

Aero‐mechanical design of high‐lift systems

Aero‐mechanical design of high‐lift systems

High-Lift Mechanism Motion Generation Synthesis Using a Metaheuristic

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