by Bindolino, G., Ghiringhelli, G., Ricci, S. and Terraneo, M.
Abstract:
This paper deals with the weight estimation of the wing box of a commercial aircraft by means of a procedure suitable for very large liners and/or unconventional configurations for which statistical data and empirical formulas may not be sufficiently reliable. Attention is focused on the need to account for aeroelastic interaction from a very preliminary stage of the design cycle. The procedure exploits the first of three levels of a multilevel structural optimization system conceived for the preliminary design of the wing primary structure and a simplified evaluation of the cross-sectional properties. The comparison between weight estimates obtained with the present procedure and predictions supplied by available literature shows a satisfactory agreement.
Reference:
Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation (Bindolino, G., Ghiringhelli, G., Ricci, S. and Terraneo, M.), In JOURNAL OF AIRCRAFT, AMER INST AERONAUT ASTRONAUT, volume 47, 2010.
Bibtex Entry:
@article{ ISI:000276565300012, Author = {Bindolino, G. and Ghiringhelli, G. and Ricci, S. and Terraneo, M.}, Title = {{Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation}}, Journal = {{JOURNAL OF AIRCRAFT}}, Year = {{2010}}, Volume = {{47}}, Number = {{2}}, Pages = {{475-489}}, Month = {{MAR-APR}}, Abstract = {{This paper deals with the weight estimation of the wing box of a commercial aircraft by means of a procedure suitable for very large liners and/or unconventional configurations for which statistical data and empirical formulas may not be sufficiently reliable. Attention is focused on the need to account for aeroelastic interaction from a very preliminary stage of the design cycle. The procedure exploits the first of three levels of a multilevel structural optimization system conceived for the preliminary design of the wing primary structure and a simplified evaluation of the cross-sectional properties. The comparison between weight estimates obtained with the present procedure and predictions supplied by available literature shows a satisfactory agreement.}}, Publisher = {{AMER INST AERONAUT ASTRONAUT}}, Address = {{1801 ALEXANDER BELL DRIVE, STE 500, RESTON, VA 22091-4344 USA}}, Type = {{Article}}, Language = {{English}}, Affiliation = {{Bindolino, G (Corresponding Author), Politecn Milan, Dipartimento Ingn Aerospaziale, Via La Masa 34, I-20156 Milan, Italy. Bindolino, G.; Ghiringhelli, G.; Ricci, S.; Terraneo, M., Politecn Milan, Dipartimento Ingn Aerospaziale, I-20156 Milan, Italy.}}, DOI = {{10.2514/1.41552}}, ISSN = {{0021-8669}}, Research-Areas = {{Engineering}}, Web-of-Science-Categories = {{Engineering, Aerospace}}, Author-Email = {{Giampiero.Bindolino@polimi.it Gianluca.Ghiringhelli@polimi.it Sergio.Ricci@polimi.it terraneo@aero.polimi.it}}, ResearcherID-Numbers = {{Ricci, Sergio/F-1093-2012 Ghiringhelli, Gian Luca/E-5797-2012 Bindolino, Giampiero/D-8516-2011}}, ORCID-Numbers = {{Ricci, Sergio/0000-0002-4613-1896 Ghiringhelli, Gian Luca/0000-0003-3474-9258 Bindolino, Giampiero/0000-0002-6990-8709}}, Number-of-Cited-References = {{34}}, Times-Cited = {{31}}, Usage-Count-Last-180-days = {{0}}, Usage-Count-Since-2013 = {{6}}, Journal-ISO = {{J. Aircr.}}, Doc-Delivery-Number = {{581ZT}}, Unique-ID = {{ISI:000276565300012}}, DA = {{2020-12-22}}, }
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