Review of the Most Important Design Optimization Technique of Composite Wing
Journal Title: INCAS BULLETIN - Year 2016, Vol 8, Issue 4
Abstract
The scope of wing optimization is to design a structure that meets all the airworthiness demands while minimizing its weight. This paper introduces a review for the most important optimization design tools of composite wings with multiple load cases and large scale design variables. Each discipline resorts to accurate design to ensure better performance. Accurate design and multidisciplinary optimization design for wings need large scale design variables. The structural design of an airframe is determined by multidisciplinary criteria (stress, fatigue, buckling, control surface effectiveness, flutter and weight etc.). Several thousands of structural sizes of stringers, panels, ribs etc. have to be determined considering hundreds of thousands of requirements to find an optimum solution, i.e. a design fulfilling all requirements with a minimum weight or minimum cost respectively.
Authors and Affiliations
Bogdan-Alexandru BELEGA, Mihai MIHAILA-ANDRES
IAR-93 military aircraft monument
In this presentation, we will concentrate on the vertical support, which is free from all sides. A Finite Element Model (FEM) of the IAR-93 aircraft monument has been developed in PATRAN/NASTRANĀ®, partly from a previous...
Disturbance observer based sliding mode control for unmanned helicopter hovering operations in presence of external disturbances
Numerous control techniques are developed for miniature unmanned helicopters to do hover operation with each method having its own advantages and limitations. During the hover operation helicopters suffer from unknown ex...
Experimental results and numerical simulations for transonic flow over the ONERA M4R model
This paper presents a comparison between experimental results of transonic flow over the ONERA M4R calibration model obtained in the INCAS Trisonic wind tunnel and the numerical results. The first purpose, emphasized in...
Development of composite aircraft components in INCDT COMOTI, Bucharest
This paper presents the recent research activities within INCDT COMOTI, in the composite materials field. The author makes a short introduction of this field and presents an example of application developed within the co...
Advanced Techniques of Stress Analysis
This article aims to check the stress analysis technique based on 3D models also making a comparison with the traditional technique which utilizes a model built directly into the stress analysis program. This comparison...