Recently, machine learning tools have been vastly used in different engineering problems.
This paper determines the composite wing aeroelastic instability boundary by an adaptive …

In this article the composite wing aeroelastic instability speed is optimized by genetic
algorithm relative to fiber angle for different layers and follower forces. Aircraft wing is …

The purpose of this study is to show the influence of fiber orientation of laminated
composites on bending-torsion coupling rigidity and Frequency analysis of aircraft wing …

The main goal of this article is to train a support vector machine in order to determine the
boundary of the composite wing aeroelastic instability. Aircraft wing is modeled as a …

The main goal of this article is to analyze the sensitivity and find the most effective property
among structural properties that have the most significant impact on the flutter velocity of a …

The increase in flexibility of modern aircraft structures requires the aeroelastic effects be
taken into consideration from the very beginning of the design phase in order to escape …

هدف از این مقاله، آموزش ماشین بردار پشتیبان برای تعیین مرز ناپایداری آیروالاستیک فلاتر
یک بال کامپوزیتی می‌باشد. بال هواپیما به صورت یک تیر دارای دو درجه آزادی و یک سر گیردار به …‎

Flutter is a catastrophic phenomenon that must be avoided and for this, the flutter speed
should be increased beyond the operational speed range. The effect of different laminate ply …

In this article, the Flutter speed of a composite wing carrying two power engines is analyzed.
The wing is modeled as a beam with two degrees of freedom, which is a cantilever, with two …

In this article the composite wing aeroelastic instability speed is optimized by genetic
algorithm relative to fiber angle for different layers and follower forces. Aircraft wing is …