Abstract
For the planned optimization of the vertical tailplane (VTP) of a Megaliner transport aircraft configuration a prior basic study is undertaken where the influence of simplifying the aircraft geometry on the characteristics of the VTP is examined. Four different configurations with varying simplification level were investigated. These are: a VTP on a base plate, a VTP on a fuselage, a VTP on a fuselage with horizontal tailplane and a VTP on a fuselage with horizontal tailplane, wing and belly fairing. Several flight cases were identified where the characteristics of the VTP are most important and then analyzed by means of numerical flow analysis using the flow solver TAU developed at the German Aerospace Center DLR. Determined are the side force coefficient generated at maximum rudder deflection, the high speed drag, the gradient of the side force coefficient due to rudder deflection and the gradient of the side force coefficient due to sideslip angle. The latter two were evaluated at low and high speed conditions. The simplified configurations were then compared to the most complete one as reference case.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Centaursoft, Homepage (2010), http://www.centaursoft.com (cited August 10, 2010)
Chen, B.H., Wellmer, G., Ballmann, J.: Numerical Prediction of Aeroelastic Effects on Twin-Sting-Rig mounted Models for Rear Fuselage and Empennage Flow Investigations in Transonic Wind Tunnel. International Forum on Aeroelasticity and Structural Dynamics (2007)
Deutsches Zentrum für Luft- und Raumfahrt e.V, Technical Documentation of the DLR TAU-Code. Technical Report, Institute of Aerodynamics and Flow Technology, DLR Braunschweig/Göttingen (2006)
Flores, R., Ortega, E., Oñate, E.: Numerical Investigation of Wind-Tunnel Model Deformations Caused by the Twin-Sting Support System. J. Aircr. 47, 708–714 (2010), doi:10.2514/1.45272
Gebhardt, L., Enk, S., Weber, C., Brezillon, J.: Numerical Optimization on the Vertical Tailplane of Transport Aircraft as part of the LuFoIV Research Project AeroNext+. Presentation 16th DGLR Fach-Symposium of STAB, RWTH Aachen (2008)
Gerhold, T.: Overview of the Hybrid RANS Code TAU. In: Kroll, N., Fassbender, J. (eds.) MEGAFLOW – Numerical Flow Simulation for Aircraft Design. NNFM, vol. 89, pp. 81–92. Springer (2005)
Pettersson, K., Rizzi, A.: Reynolds Number Effects Identified with CFD Methods Compared to Semi-Empirical Methods. In: ICAS 2006-2.3.4, p. 14 (2006)
Rotta, J.: Luftkräfte am Tragflügel mit einer seitlichen Scheibe. Ingenieur-Archiv XIII 3, 119–131 (1942)
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2013 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
Kröhnert, A., Gebhardt, L. (2013). Investigation of the Impact of Simplifying the Aircraft Geometry on the Characteristics of the Vertical Tailplane. In: Dillmann, A., Heller, G., Kreplin, HP., Nitsche, W., Peltzer, I. (eds) New Results in Numerical and Experimental Fluid Mechanics VIII. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 121. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-35680-3_1
Download citation
DOI: https://doi.org/10.1007/978-3-642-35680-3_1
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-35679-7
Online ISBN: 978-3-642-35680-3
eBook Packages: EngineeringEngineering (R0)