Aerodynamic Analysis and Parametric Study of the Blended-Wing-Body-Type Business Jet
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Abstract
The market demand on business jets is growing fast. The Blended-Wing-Body (BWB) configuration is adapted to design high-efficient green business jet. Conceptual study of the BWB-type transonic business jet is carried out. The BWB-type business jet expected to provide a better cabin space and aerodynamic performance to compare with the conventional business jet. An aerodynamic analysis of the BWB-type transonic business jet is performed to understand the flow field around the aircraft at a high subsonic flight speed. The commercial CFD (Computational Fluid Dynamics) code, ANSYS Fluent, is used for aerodynamic analysis. A parametric study is carried out to analyze the relation between the design parameters and aerodynamic characteristics. The commercial PIDO (Process Integration and Design Optimization) tool, PIAnO, is used to perform a parametric study. As a result of parametric study, the sensitivity of the design parameters is analyzed and a proportion of aerodynamic influence of each design parameter is presented. One of the sample design configurations for detailed aerodynamic analysis is selected. As a result of the aerodynamic analysis, aerodynamic coefficients and pressure coefficient distribution around the BWB-type business jet are presented. Increase of AOA and Mach number produces stronger shock and drag coefficient is increased due to wave drag.
Keywords
Blended-wing-body Business jet Aerodynamic analysis Parametric studyNotes
Acknowledgements
The authors appreciate PIDOTECH Inc.’s supporting PIAnO software as a PIDO tool for the design of experiments and parametric study.
References
- 1.“Market Forecast 2013-2032” (2013) Bombardier aerospaceGoogle Scholar
- 2.Potsdam MA (1997) Blended wing body analysis and design. AIAA Appl Aerodyn Conf 799–805Google Scholar
- 3.Liebeck RH, Page MA, Rawdon BK (1998) Blended-wing-body subsonic commercial transport. In: 36th AIAA aerospace sciences meeting and exhibitGoogle Scholar
- 4.Osterheld CM, Heinze W, Horst P (2001) “Preliminary design of a blended wing body configuration using the design tool PrADO. DGLR BERICHT, no. 5, pp 119–128Google Scholar
- 5.Qin N, Vavalle A, Le Moigne A, Laban M, Hackett K, Weinerfelt P (2004) Aerodynamic considerations of blended wing body aircraft. Prog Aerosp Sci 40(6):321–343. https://doi.org/10.1016/j.paerosci.2004.08.001 CrossRefGoogle Scholar
- 6.Liebeck RH (2004) Design of the blended wing body subsonic transport. J Aircr 41(1):10–25. https://doi.org/10.2514/1.9084 CrossRefGoogle Scholar
- 7.Qin N, Vavalle A, Le Moigne A (2005) Spanwise lift distribution for blended wing body aircraft. J Aircr 42(2):356–365CrossRefGoogle Scholar
- 8.Dowling AP, Hynes T (2006) Towards a silent aircraft. Aeronaut J 110(1110):487–494CrossRefGoogle Scholar
- 9.Hileman JI, Spakovszky ZS, Drela M (2007) Airframe design for silent aircraft. In: 45th AIAA aerospace science meeting and exhibit, Reno, NevadaGoogle Scholar
- 10.Kim HD, Brown GV, Felder JL (2008) Distributed turboelectric propulsion for hybrid wing body aircraft. In: 2008 international powered lift conference, London, UKGoogle Scholar
- 11.Felder J, Kim HD, Brown G (2009) Turboelectric distributed propulsion engine cycle analysis for hybrid wing body aircraft. In: 47th AIAA aerospace science meeting, Orlando, FLGoogle Scholar
- 12.Leifsson L, Ko A, Mason WH, Schetz JA, Grossman B, Haftka RT (2013) Multidisciplinary design optimization of blended-wing-body transport aircraft with distributed propulsion. Aerosp Sci Technol 25(1):16–28CrossRefGoogle Scholar
- 13.Nara T, Kanazaki M (2010) Initial design and evaluation of a novel concept regional aircraft. In: 2010 Asia-Pacific international symposium on aerospace technology, 2010Google Scholar
- 14.Kanazaki M, Hanida R, Nara T, Shibata M, Nomura T, Murayama M, Yamamoto K (2013) Challenge of design exploration for small blended wing body using unstructured flow solver. Comput Fluids 85:71–77CrossRefGoogle Scholar
- 15.Harijono D, Alvin KLW (2012) Conceptual design and aerodynamic study of blended wing body business jet. In: Proceeding of 28th international congress of the aeronautical sciences, Brisbane, 2012Google Scholar
- 16.Mulyanto T, Nurhakim MLI (2013) Conceptual design of blended wing body business jet aircraft. J Kones 20:299–306Google Scholar
- 17.PIAnO (Process Integration, Automation and Optimization). User’s manual, version 3, PIDOTECH IncGoogle Scholar
- 18.Schmitt V, Charpin F (1979) Pressure distributions on the ONERA-M6-wing at transonic mach numbers. In: Experimental data base for computer program assessment, report of the fluid dynamics panel working group 04, AGARD AR 138Google Scholar