review of the most important design optimization technique of composite wing

Clicks: 93
ID: 233910
2016
Free PDF
Article Quality & Performance Metrics
Overall Quality
Not rated
Combines reader engagement with the AI quality analysis. This article has not been analysed, so there is no overall score — reader engagement is measured and shown alongside.
AI Quality Assessment
Not analyzed
Readership in this journal
Emerging

Ranked #27 of 32 articles by views in biotechnology letters

Most read Least read

Bar heights use a square-root scale.

Mint this article as an NFT
Not yet minted

Create a permanent, verifiable on-chain record of this article on the Scimatic Network. The NFT is held in your Journament account, and you can withdraw it to your own wallet at any time.

5 SUSD one-off · no wallet required
Sign in to mint
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.
Reference Key
belega2016incasreview Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;Bogdan-Alexandru BELEGA;Mihai MIHAILA-ANDRES
Journal biotechnology letters
Year 2016
DOI
10.13111/2066-8201.2016.8.4.5
URL
http://bulletin.incas.ro/files/belega__mihaila-andres_vol_8_iss_4.pdf
Keywords
airfoil astronautics aeronautics optimization techniquemotor vehicles

Citations

No citations found. To add a citation, contact the admin at info@scimatic.org

Comments

No comments yet. Be the first to comment on this article.