Multi-Objective Optimization of Conventional Airplane Vertical Tail and Rudder

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Karimi Jalal; Chegeni Mohsen

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Paper Information

Journal: JOURNAL OF AERONAUTICAL ENGINEERING (JOAE) Year:2019 | Volume:21 | Issue:1 Page(s): 35-43

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Title

Multi-Objective Optimization of Conventional Airplane Vertical Tail and Rudder

Author(s)

Karimi Jalal | Chegeni Mohsen | Issue Writer Certificate

Keywords

Vertical tail and rudderQ1

flying qualityQ1

Dynamic stabilityQ2

Spin recoveryQ1

Trim abilityQ1

multi-objective optimizationQ1

Abstract

In the present article, with the aim to upgrading operational capabilities of existing flying vehicles, a method is proposed to simultaneously optimize the Vertical tail and rudder of a conventional airplane. To this end, all the design requirements of this important part of the configuration have been formulated in the context of a constrained multi-objective optimization problem. The ability to calculate aerodynamic coefficients and mass parameters have been created, when airplane geometry is varying. In this way, for sensitivity purposes, the effect of the geometric parameters of the configuration on the flying qualities and performance characteristics of the airplane can be obtained. Also, in optimization purposes, one part of the configuration can be optimized, while the reciprocal effects of all the configuration components is taken into account. The problem is solved by combining the non-dominated sorting genetic algorithm with the feasibility tournament approach.

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APA: Copy

Karimi, Jalal, & Chegeni, Mohsen. (2019). Multi-Objective Optimization of Conventional Airplane Vertical Tail and Rudder. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 21(1 ), 35-43. SID. https://sid.ir/paper/370187/en

Vancouver: Copy

Karimi Jalal, Chegeni Mohsen. Multi-Objective Optimization of Conventional Airplane Vertical Tail and Rudder. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2019;21(1 ):35-43. Available from: https://sid.ir/paper/370187/en

IEEE: Copy

Jalal Karimi, and Mohsen Chegeni, “Multi-Objective Optimization of Conventional Airplane Vertical Tail and Rudder,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 21, no. 1 , pp. 35–43, 2019, [Online]. Available: https://sid.ir/paper/370187/en

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