D and DD-drop layup optimization of aircraft wing panels under multi-load case design environment. (15th September 2020)
- Record Type:
- Journal Article
- Title:
- D and DD-drop layup optimization of aircraft wing panels under multi-load case design environment. (15th September 2020)
- Main Title:
- D and DD-drop layup optimization of aircraft wing panels under multi-load case design environment
- Authors:
- Shrivastava, Sachin
Sharma, Naresh
Tsai, Stephen W.
Mohite, P.M. - Abstract:
- Abstract: The aerospace industry is on a perpetual drive to optimize structures with developments in modeling and analysis capabilities. The traditionally used laminates with 0 °, 90 °, ± 45 ° orientations are called Legacy QUAD Laminates (LQL). The recent discovery of Trace of an orthotropic stress tensor A allows reduction of design variables by the replacement of LQL with equivalent stiffness DD 1 (double-double) laminate having self-repeating orientations in a set of ± ϕ / ± ψ . The optimized LQL structures are with mid-plane symmetry, excessive ply-migrations, and variability in ply-orientations, which make the manufacturing process cumbersome. On the other hand, DD-laminates are simplified, thinner and free from mid-plane symmetry, thus enable ten-fold reduction in production resources. The present study, an artificial intelligent (AI) genetic-algorithm based stochastic optimizer replaces LQL with DD-laminates, which follows DD-drop design for mass optimization. The optimization algorithm works with unit-circle failure, buckling mode, and wing-tip deflection design criteria and derives optimal-wing with lowest mass, well suited for design requirements in multiple design load-case. The application of algorithm shows 68–70% mass reduction to an initial full-length ply wing-box model of LQL. The minimization of ply-migrations by D/DD-drop optimization yields structures with better resistance for delamination and well suited for automated production.
- Is Part Of:
- Composite structures. Volume 248(2020)
- Journal:
- Composite structures
- Issue:
- Volume 248(2020)
- Issue Display:
- Volume 248, Issue 2020 (2020)
- Year:
- 2020
- Volume:
- 248
- Issue:
- 2020
- Issue Sort Value:
- 2020-0248-2020-0000
- Page Start:
- Page End:
- Publication Date:
- 2020-09-15
- Subjects:
- DD-drop -- Composite wing-box optimization -- Unit circle failure criterion -- Mid-plane symmetry -- Laminate homogenization
Composite construction -- Periodicals
Composites -- Périodiques
624.18 - Journal URLs:
- http://www.sciencedirect.com/science/journal/02638223 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.compstruct.2020.112518 ↗
- Languages:
- English
- ISSNs:
- 0263-8223
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 3364.970000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 13591.xml