Abstract
This report presents a multi-disciplinary optimization (MDO) process that minimizes the mission fuel burn of an aeroelastic long-range transport aircraft configuration, by modifying the wing planform, twist, and structural element thicknesses. Two optimizations are performed, one where the fuel burn is approximately evaluated through Breguet range equation, and the other where the ordinary differential equation (ODE) for the step-climb cruise is formally integrated. This is done in order to determine if the Breguet equation is still sufficient in face of high-fidelity aeroelastic simulations. The two optimized designs ended up having similar improvements, thus confirming the applicability of the Breguet equation, for the number of design parameters that were employed.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Becker, R.G., Wolters, F., Nauroz, M., Otten, T.: Development of a gas turbine performance code and its application to preliminary engine design. In: Deutscher Luft- und Raumfahrtkongress 2011 (2011)
Ciampa, P.D., Nagel, B., Rajpal, D., Rocca, G.L.: Preliminary design for flexible aircraft in a collaborative environment. In: 4th CEAS Air and Space Conference (2013)
Freund, S., Heinecke, F., Führer, T., Willberg, C.: Parametric model generation and sizing of lightweight structures for a multidisciplinary design process. In: NAFEMS DACH-Tagung (2014)
Führer, T., Willberg, C., Freund, S., Heinecke, F.: Parametric model generation and automated sizing process for the analysis of aircraft structures using the design environment DELiS. In: 4th European Aeronautics Science Network International Workshop (2014)
Kenway, G.K.W., Martins, J.R.R.A.: Multipoint high-fidelity aerostructural optimization of a transport aircraft configuration. J. Aircraft 51 (2014). doi:10.2514/1.C032150
Kroll, N., et al.: DLR-Projekt Digital-X: Auf dem Weg zur virtuellen Flugzeugentwicklung und Flugerprobung auf Basis höherwertiger Verfahren. In: Deutscher Luft- und Raumfahrtkongress 2014, DLRK2014-340099 (2014)
Lefebvre, T., Schmollgruber, P., Blondeau, C., Carrier, G.: Aircraft conceptual design in a multi-level, multi-fidelity, multi-disciplinary optimization process. In: 28th Congress of the International Council of the Aeronautical Sciences (2012)
Liem, R.P., Kenway, G.K.W., Martins, J.R.R.A.: Multimission aircraft fuel burn minimization via multipoint aerostructural optimization. AIAA J. 53 (2015). doi:10.2514/1.J052940
Liersch, C., Hepperle, M.: A distributed toolbox for multidisciplinary preliminary aircraft design. CEAS Aeronaut. J. 2(1) (2011)
Martins, J.R.R.A., Alonso, J.J., Reuther, J.J.: A coupled-adjoint sensitivity analysis method for high-fidelity aero-structural design. Optim. Eng. 6(1) (2005). doi:10.1023/B:OPTE.0000048536.47956.62
Meinel, M., Einarsson, G.O.: The FlowSimulator framework for massively parallel CFD applications. In: Para 2010 (2010)
Moerland, E., Zill, T., Nagel, B., Spangenberg, H., Schumann, H., Zamov, P.: Application of a distributed MDAO framework to the design of a short- to medium-range aircraft. In: Deutscher Luft- und Raumfahrtkongress (2012)
Piperni, P., DeBlois, A., Henderson, R.: Development of a multilevel multidisciplinary-optimization capability for an industrial environment. AIAA J. 51(10) (2013)
Ronzheimer, A., Natterer, F.J., Brezillon, J.: Aircraft wing optimization using high fidelity closely coupled CFD and CSM methods. In: 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference (2010)
Rowan, T.H.: Functional stability analysis of numerical algorithms. Ph.D. thesis, University of Texas at Austin (1990)
Schuhmacher, G., Daoud, F., Petersson, O., Wagner, M.: Multidisciplinary airframe design optimisation. In: 28th Congress of the International Council of the Aeronautical Sciences (2012)
Schwamborn, D., Gerhold, T., Heinrich, R.: The DLR TAU-Code: Recent applications in research and industry. In: ECCOMAS CFD 2006 (2006)
Seider, D., Basermann, A., Mischke, R., Siggel, M., Tröltzsch, A., Zur, S.: Ad-hoc collaborative design with focus on iterative multidisciplinary process chain development applied to thermal management of spacecraft. In: 4th CEAS Air and Space Conference (2013)
Seider, D., Fischer, P., Litz, M., Schreiber, A., Gerndt, A.: Open source software framework for applications in aeronautics and space. In: IEEE Aerospace Conference (2012)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2016 Springer International Publishing Switzerland
About this paper
Cite this paper
Ilić, Č. et al. (2016). Comparison of Breguet and ODE Evaluation of the Cruise Mission Segment in the Context of High-Fidelity Aircraft MDO. In: Dillmann, A., Heller, G., Krämer, E., Wagner, C., Breitsamter, C. (eds) New Results in Numerical and Experimental Fluid Mechanics X. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 132. Springer, Cham. https://doi.org/10.1007/978-3-319-27279-5_8
Download citation
DOI: https://doi.org/10.1007/978-3-319-27279-5_8
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-27278-8
Online ISBN: 978-3-319-27279-5
eBook Packages: EngineeringEngineering (R0)