Issue |
Mechanics & Industry
Volume 22, 2021
Advances of junior researchers in aerospace sciences: a focus on innovative design
|
|
---|---|---|
Article Number | 39 | |
Number of page(s) | 19 | |
DOI | https://doi.org/10.1051/meca/2021037 | |
Published online | 08 July 2021 |
- European Commission, Flightpath 2050: Europe's Vision for Aviation. European Commission, Directorate General for Research and Innovation, Directorate General for Mobility and Transport (2011) [Google Scholar]
- D.S. Lee, G. Pitari, V. Frewe, K. Gierens et al, Transport impacts on atmosphere and climate: aviation, Atmos. Environ. 44, 4678–4734 (2010) [CrossRef] [Google Scholar]
- O. Dessens, M.O. Köhler, H.L. Rogers, R.L. Jones, J.A. Pyle, Aviation and climate change, Transp. Policy 34, 14–20 (2014) [Google Scholar]
- Eurocontrol, European Aviation in 2040, Challenges of Growth, Annex 1, Flight Forecast to 2040 (2018) [Google Scholar]
- Airbus, Cities, Airports & Aircraft - 2019–2038, Global Market Outlook (2019) [Google Scholar]
- A.L. Tasca, V. Cipolla, K. Abu Salem, M. Puccini, Innovative box-wing aircraft: emissions and climate change, Sustainability 13, 3282 (2021) [Google Scholar]
- B. Brelje, J. Martins, Electric, hybrid, and turboelectric fixed-wing aircraft: A review of concepts, models, and design approaches, Progr. Aerospace Sci. 104, 1–19 (2019) [Google Scholar]
- C. Pornet, A. Isikveren, Conceptual design of hybrid-electric transport aircraft, Progr. Aerospace Sci. (2015) [Google Scholar]
- G. Palaia, D. Zanetti, K. Abu Salem, V. Cipolla, V. Binante, THEA-CODE: a design tool for the conceptual design of hybrid-electric aircraft with conventional or unconventional airframe configurations, Mech. Ind. 22, 19 (2021) [Google Scholar]
- D. Schmitt, Challenges for unconventional transport aircraft configurations, Air Space Europe 3, 67–72 (2001) [Google Scholar]
- IATA, Aircraft Technology Roadmap to 2050, Report (2020) [Google Scholar]
- C. Werner-Westphal, W. Heinze, P. Horst, Multidisciplinary integrated preliminary design applied to unconventional aircraft configurations, J. Aircraft 45, 2 (2008) [Google Scholar]
- R.H. Liebeck, Design of the blended wing body subsonic transport, J. Aircraft 41, 1 (2004) [Google Scholar]
- N. Qin, A. Vavalle, A. Le Moigne, M. Laban, K. Hackett, P. Weinerfelt, Aerodynamic considerations of blended wing body aircraft, Progr. Aerospace Sci. 40, 321–343 (2004) [Google Scholar]
- J. Wolkovitch, The joined wing: an overview, J. Aircraft 23, 3 (1986) [Google Scholar]
- R. Cavallaro, L. Demasi, Challenges, ideas, and innovations of joined-wing configurations: a concept from the past, an opportunity for the future, Progr. Aerospace Sci. 87, 1–93 (2016) [Google Scholar]
- L. Prandtl, Induced drag of multiplanes, NACA-TN-182 (1924), url: https://ntrs.nasa.gov/search.jsp?R=19930080964 [Google Scholar]
- A. Frediani, G. Montanari, Best wing system: an exact solution of the Prandtl's problem, in Variational Analysis and Aerospace Engineering, Springer Optimization and Its Applications (Springer, 2009), vol 33, 183–211 [Google Scholar]
- A. Frediani, V. Cipolla, E. Rizzo, The PrandtlPlane configuration: overview on possible applications to civil aviation, variational analysis and aerospace engineering: mathematical challenges for aerospace design, in Springer Optimization and Its Applications (Springer, 2012), vol 66, 179–210 [Google Scholar]
- A. Frediani, V. Cipolla, F. Oliviero, IDINTOS: the first prototype of an amphibious PrandtlPlane-shaped aircraft, Aerotecnica Missili Spazio 99, 233–249 (2016) [Google Scholar]
- A. Frediani, V. Cipolla, F. Oliviero, Design of a prototype of light amphibious PrandtlPlane, in 56th AIAA /ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA SciTech Forum, Kissimmee, Florida, 2015 [Google Scholar]
- PARSIFAL Project, website, www.parsifalproject.eu [Google Scholar]
- M. Kousolidou, D. Violato, Towards Climate-Neutral Aviation, European Commission Technical Report (2020) [Google Scholar]
- A. Frediani, V. Cipolla, K. Abu Salem, V. Binante, M.P. Scardaoni, Conceptual design of PrandtlPlane civil transport aircraft, Proc. Inst. Mech. Eng. G 234–10, 1675–1687 (2019) [Google Scholar]
- E. Rizzo, A. Frediani, Application of optimisation algorithms to aircraft aerodynamics, in Variational Analysis and Aerospace Engineering. Springer Optimization and Its Applications (Springer, 2009), vol. 33, 419–446 [Google Scholar]
- E. Rizzo, Optimization Methods Applied to the preliminary design of innovative non conventional aircraft configurations, Ph.D. Thesis, University of Pisa, 2009 [Google Scholar]
- E.F. Curtis, M.L. Overton, A sequential quadratic programming algorithm for nonconvex, nonsmooth constrained optimization, SIAM J. Optim. 22, 474–500 (2012) [CrossRef] [Google Scholar]
- S.P. Han, A globally convergent method for nonlinear Programming, J. Optim. Theory Appl. 22, 297–309 (1977) [Google Scholar]
- B. Addis, M. Locatelli, F. Schoen, Local optima smoothing for global optimization, Optim. Methods Softw. 20, 417–437 (2005) [Google Scholar]
- AVL (Athena Vortex Lattice), Version 3.36, website, url: http://web.mit.edu/drela/Public/web/avl/ [Google Scholar]
- V. Cipolla, A. Frediani, K. Abu Salem, V. Binante, E. Rizzo, M. Maganzi, Preliminary transonic CFD analyses of a PrandtlPlane transport aircraft, Transp. Res. Proc. 29, 82–91 (2018) [Google Scholar]
- M. Carini, M. Meheut, S. Kanellopoulos, V. Cipolla, K. Abu Salem, Aerodynamic analysis and optimization of a boxwing architecture for commercial airplanes, AIAA SciTech Forum, Orlando (2020) [Google Scholar]
- D.P. Raymer, Aircraft Design: A Conceptual Approach, AIAA Education Series (1992) [Google Scholar]
- Association of European Airlines, AEA, Short-Medim Range Aircraft AEA Requirements, Report G(T) 5656 (1987) [Google Scholar]
- W.H. Mason, Analytic models for technology integration in aircraft design, in AIAA Aircraft Design, Systems and Operations Conference, Dayton, 1990 [Google Scholar]
- M. Beltramo, D. Trapp, B. Kimoto, D. Marsh, Parametric study of transport aircraft systems cost and weight, NASA Report CR151970, 1977 [Google Scholar]
- F. Oliviero, Preliminary design of a very large PrandtlPlane freighter and airport network analysis, Ph.D. Thesis, University of Pisa, 2015 [Google Scholar]
- L. Cappelli, G. Costa, V. Cipolla, A. Frediani, F. Oliviero, E. Rizzo, Aerodynamic optimization of a large PrandtlPlane configuration, Aerotecnica Missili Spazio 95, 163–175 (2016) [Google Scholar]
- V. Cipolla, A. Frediani, K. Abu Salem, M. Picchi Scardaoni, A. Nuti, V. Binante, Conceptual design of a box wing aircraft for the air transport of the future, AIAA Aviation Forum, Atlanta (2018) [Google Scholar]
- K. Abu Salem, V. Cipolla, M. Carini, M. Méheut, S. Kanellopoulos, V. Binante, M. Maganzi, Aerodynamic design and preliminary optimization of a commercial PrandtlPlane aircraft, in Proceedings of 8th EUCASS Conference, Madrid , 2019 [Google Scholar]
- V. Cipolla, K. Abu Salem, M. Picchi Scardaoni, V. Binante, Preliminary design and performance analysis of a box-wing transport aircraft, in AIAA SciTech Forum, Orlando , 2020 [Google Scholar]
- D.A. van Ginneken, M. Voskuijl, M.J. van Tooren, A. Frediani, Automated Control Surface Design and Sizing for the Prandtl Plane, in AIAA SciTech Forum, 51th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Orlando , 2010 [Google Scholar]
- E. Torenbeek, Synthesis of subsonic airplane design (Springer, Netherlands, 1982) [Google Scholar]
- K. Abu Salem, G. Palaia, M. Bianchi, D. Zanetti, V. Cipolla, V. Binante, Preliminary take-off analysis and simulation for a PrandtlPlane commercial aircraft, Aerotecnica Missili Spazio 99, 203–216 (2020) [Google Scholar]
- J. Sun, J.M. Hoeckstra, J. Ellerbroek, Aircraft Drag Polar Estimation Based on a Stochastic Hierarchical Model, Eighth SESAR Innovation Days, (2018) [Google Scholar]
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