Mathematical Modeling of the Design Process of Additional Aerodynamic Surfaces of the Wing as a Component of the Configuration of a Commercial Airliner

Authors

  • Aleksandr Gorbunov Federal State Educational Government-financed Institution of Higher Professional Education “Orenburg State University”, Orenburg, Russia
  • Aleksej Pripadchev Federal State Educational Government-financed Institution of Higher Professional Education “Orenburg State University”, Orenburg, Russia
  • Irina Bykova Federal State Educational Government-financed Institution of Higher Professional Education “Orenburg State University”, Orenburg, Russia

Keywords:

Additional aerodynamic surfaces, wing-tip mounted winglets, mathematical modelling, parametric synthesis, commercial airliner, structural optimization, automation of conceptual design, development and design procedures, model of characteristics

Abstract

This paper introduces the methodology and the method of automated configuration design for the additional aerodynamic surfaces of the wing as a component of a commercial airliner’s configuration, based on the suggested mathematical model. The mathematical model allows to carry out a particular task of developing and designing the additional aerodynamic surface of the wing for a commercial airliner, as well as to select the required type of the additional aerodynamic surface for a certain aircraft. The decision on the required type of the additional aerodynamic surface for a certain aircraft is made by utilizing a specialized software product, where a multi-criterial approach to the selection of the method is implemented, when defining the tasks chosen. The automation of the design process for the additional aerodynamic surfaces of the wing as a component of a commercial airliner’s configuration is achieved by means of the software product that we have devised, written in an object-oriented high-level programming language.

References

KOMAROV, V. А. et al. Aircraft conceptual design: a study guide(In Russian),ed. 2.Samara : The Samara State Aerospace University Press,2013.

The ontology of design.The new equipment Publishers, 2013.

RAYMER, D.P. Aircraft Design: A Conceptual Approach.Washington:American Institute of Aeronautics and Astronautics, 1992.

AOKI, М.,Introduction to the methods of optimization(In Russian).Мoscow: Science, 1977.

BELOTSERKOVSKY,A.S. Creating and applying the mathematical models of airplanes(In Russian).Мoscow: Science, 1984.

AHO, A.V.,HOPCROFT,D.andULMAN D.J.Data structure and algorithms(In Russian).Мoscow: The Williams Publishing house, 2000.

KEYSLER, G.andCHAN,C.C.The theory of models(In Russian).Мoscow: Machinebuilding, 1997.

KENNEDY,G.J. Aerostructural analysis and design optimization of composite aircraft[PhD Thesis].Toronto: University of Toronto, 2012.

PEREZ,R., JANSEN,P.andMARTINS,J. Aero-Structural Optimization of Non-Planar Lifting Surface Configurations. InProceedings of the 12thAIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008.

HEPPERLE, M.&andSTRUBER, H.Optimization of Flying Wing Transport Aircraft: DLR-Interner Bericht.Braunschweig:Institut für Aerodynamik und Strömungstechnik, 2005.

TORENBEEK, E. Synthesis of Subsonic Airplane Design.Delft University Press, 1982.

SCHIKTANZ, D.ConceptualDesign of a Medium Range Box Wing Aircraft[Master Thesis].Hamburg:HAW Hamburg, Department Fahrzeug technik und Flugzeugbau, 2011.

WHITCOMB,R.A Design Approach and Selected Wind-Tunnel results at High Subsonic Speeds for Wing-Tip Mounted Winglets.Langley Research Center, 1976.

KOMAROV, V.А.andKUZNETSOV,А.S. Selecting an aircraft's configuration using the technology of multi-disciplinary optimization: an electronic study guide(In Russian).Samara:The Samara State Aerospace University named after S. P. Korolev, 2012.

NAGEL,B., KINTSCHER, M. andSTREIT,T.Active and Passive Structural Measures for Aeroelastic Winglet Design.ICAS, 2008.

GORBUNOV,А.А.andPRIPADCHEV,А.D. The software program for calculating the efficiency index of an aircraft with additional aerodynamic surfaces: the certificate of the official registration of a computer program.Certificate No. 2013613814 of the Russian Federation.The applicant and the patent-holder is a State educational institution –the Orenburg State University; appl. 01.03.2013; registered on 16.04.2013.

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Published

29-06-2016

How to Cite

Gorbunov, A., Pripadchev, A., & Bykova, I. (2016). Mathematical Modeling of the Design Process of Additional Aerodynamic Surfaces of the Wing as a Component of the Configuration of a Commercial Airliner. Advances in Military Technology, 11(1), 29–42. Retrieved from https://www.aimt.cz/index.php/aimt/article/view/1098

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Research Paper

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