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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