Advances in aircraft and spacecraft science

  • 제1권1호
  • /
  • Pages.43-67
  • /
  • 2014
  • /
  • 2287-528X(pISSN)
  • /
  • 2287-5271(eISSN)
테크노프레스 (Techno-Press)
권호 표지
DOI QR코드

DOI QR Code

Adaptable conceptual aircraft design model

  • Fioriti, Marco (Department Mechanical and Aerospace Engineering, Politecnico di Torino)
  • 투고 : 2013.02.22
  • 심사 : 2013.09.01
  • 발행 : 2014.01.31
⟨ 이전 논문 다음 논문 ⟩

초록

This paper presents a new conceptual design model ACAD (Adaptable Conceptual Aircraft Design), which differs from the other models due to its considerable adaptability to the different classes of aircraft. Another significant feature is the simplicity of the process which leads to the preliminary design outputs and also allowing a substantial autonomy in design choices. The model performs the aircraft design in terms of total weight, weight of aircraft subsystems, airplane and engine performances, and basic aircraft configuration layout. Optimization processes were implemented to calculate the wing aspect ratio and to perform the design requirements fulfillment. In order to evaluate the model outcomes, different test cases are presented: a STOL ultralight airplane, a new commuter with open-rotor engines and a last generation fighter.

키워드

참고문헌

  1. Antona, E. Chiesa, S. Corpino, S. and Viola, N. (in Italian) (2009), "L'avamprogetto dei velivoli", Atti dell'Accademia delle Scienze di Torino
  2. Azamatov, A. Woo-Lee, J. and Byun, Y.H. (2012),"Comprehensive aircraft configuration design tool for integrated product and process development", Elsevier Adv. in Engi. Software, 42,35-49
  3. Chiesa, S. (in Italian) (1977), "Sulla previsione del peso degli impianti di bordo nella fase preliminare del progetto dei velivoli", Ingegneria, $n^{\circ}1-2$.
  4. Chiesa, S. Borello, L. and Maggiore P. (2000), "An academic experience about aircraft design: affordable advanced jet trainer", Proceeding of 2000 22nd ICAS Congress, Harrogate, UK, August-September.
  5. Chiesa, S. Corpino, S. Maggiore, P. and Pasquino, M. (2000), "The weight estimation in aerospace engineering at the Polytechnic of Turin", Proceeding of 2000 SAWE Europe Conference, Bremen, November.
  6. Chiesa, S. and Maggiore, P. (1995), "Conceptual design in aeronautics: an academic viewpoint", Proceeding of '95 ICED 10th, Praga, August.
  7. Chiesa, S. Fioriti, M. and Viola, N. (2012), Methodology for an Integrated Definition of a System and Its Subsystems: The Case-Study of an Airplane and Its Subsystems Chapter of the book: Sys. Engi. - Practice and Theory, ISBN: 978-953-51-0322-6, INTECH
  8. Chiesa, S. and Viola, N. (2007), "Sub-systems equipments weight and volume first estimation; a tool for aircraft conceptual design", Int' J. Mech. Control, 8(1),813-820
  9. Jenkinson, L.R. Simpkin, P. and Rhodes, D. (1999), Civil Jet Aircraft Design (2nd Edition), American Institute of Aeronautics and Astronautics, Reston, VA.
  10. Lee, D.S. Fahey, D.W. Forster, P.M. Newton, P.J. Wit, R.C.N. Lim, L.L. Owen, B. and Sausen, R. (2009), "Aviation and global climate change in the 21st century", Elsevier Atmosferic Envi., 43(22-23),3520-3537 https://doi.org/10.1016/j.atmosenv.2009.04.024
  11. Lombardi, G. Mengali, G. and Beux F. (2006), "A hybrid genetic based optimization procedure for aircraft conceptual analysis", J. Optim. Engi., 7(2), 151-171 https://doi.org/10.1007/s11081-006-6837-1
  12. McDonald, C.F. Massardo, A.F. Rodgers, C. and Stone, A. (2008), "Recuperated gas turbine aeroengines, part II: engine design studies following early development testing", Aircraft Engi. Aerospace Tech., 80 (3), 280- 294 https://doi.org/10.1108/00022660810873719
  13. Raymer, D.P. (2012), Aircraft Design: A Conceptual Approach (5thEdition), American Institute of Aeronautics and Astronautics, Washington, DC.
  14. Roskam, J. (2003), Airplane Design Part I: Preliminary Sizing of Airplanes (2ndEdition), DARcorporation, Lawrence, KS.
  15. Saha, U. K. Mitra, M. Menon, S. J. John, N. T. Gajapathi, S. S. and Behera P. (2008), "Preliminary design analysis of a lightweight combat aircraft", Proce. the Insti. Mech. Engi., Part G: J. Aerospace Engi., 222, 507-513 https://doi.org/10.1243/09544100JAERO256

피인용 문헌

  1. Development of a new conceptual design methodology for parallel hybrid aircraft 2019, https://doi.org/10.1177/0954410017745569
  2. The advantages of a hybrid piston prop aircraft vol.20, pp.2, 2016, https://doi.org/10.3846/16487788.2016.1198093
  3. The educational experience at Politecnico di Torino to develop and increase the capability in aircraft layout comprehension and definition vol.21, pp.1, 2017, https://doi.org/10.3846/16487788.2016.1200850
  4. Trade off studies of hybrid-electric aircraft by Fuzzy Logic methodology 2018, https://doi.org/10.3233/JAE-172293
  5. Shift Steering Control of 2-axis ARM Helicopter based on a Neural Network vol.21, pp.7, 2015, https://doi.org/10.5302/J.ICROS.2015.15.0033
  6. Solving design optimization problems via hunting search algorithm with Levy flights vol.52, pp.2, 2014, https://doi.org/10.12989/sem.2014.52.2.351
  7. Development of a multidisciplinary design optimization framework for an efficient supersonic air vehicle vol.2, pp.1, 2015, https://doi.org/10.12989/aas.2015.2.1.017
  8. MALE UAV and its systems as basis of future definitions vol.88, pp.6, 2016, https://doi.org/10.1108/AEAT-08-2014-0131
  9. Possible hybrid propulsion configuration for transport jet aircraft vol.20, pp.3, 2016, https://doi.org/10.3846/16487788.2016.1200849
  10. Preliminary Sub-Systems Design Integrated in a Multidisciplinary Design Optimization Framework vol.249, pp.2017, 2014, https://doi.org/10.2478/tar-2017-0025
  11. Geometrical parameters optimizations of scarf and double scarf bounded joint vol.5, pp.3, 2014, https://doi.org/10.12989/aas.2018.5.3.401
  12. Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations vol.92, pp.5, 2014, https://doi.org/10.1108/aeat-05-2019-0109
  13. Innovative Multiple Matching Charts approach to support the conceptual design of hypersonic vehicles vol.234, pp.12, 2020, https://doi.org/10.1177/0954410020920037