Abstract
Surface generation software is being created with emphasis on parametric description of aircraft components and their junction. Applications are illustrated and examples are shared with project partners for their development of CFD mesh generation. Industry partners in the meantime and within this collaboration use this approach to develop a powerful tool for transport aircraft component design, establishing practical interaction between a theoretical aerodynamics group and the project design engineers.The goal is shaping geometry generator codes to become fast interactive tools supporting the use of aerodynamic knowledge bases in future design expert systems using modern graphic workstations.
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
Sobieczky, H., ‘Geometry Generation for Transonic Design’, Recent Advances in Numerical Methods in Fluids, Vol. 4, Ed. W. G. Habashi, Swansea: Pineridge Press, pp. 163–182. (1985).
Barnewitz, H., Becker, K., ‘Interactive Netzgenerierung mit dem algebraischen Netzgenerator INGRID - Hinweise zur Benutzung’, MBB - Bericht No. 1666, (1988).
Sobieczky, H., Stroeve, J. C.: `Generic Supersonic and Hypersonic Configurations’, AIAA91–3301, (1991)
Sobieczky, H., Hefer, G., Tusche, S.:DFVLR-F5 Test Wing Experiment for Computational Aerodynamics. Notes on Numerical Fluid Mechanics, Vol. 22, pp.4–22, ed. W. Kordulla (1988)
Sobieczky, H.: `DLR-F5 Test Wing Configuration for Computational and Experimental Aerodynamics’, Wing Surface Generator Code, Control Surface and Boundary Conditions. Report prepared for B/E Area 5 Aeronautics Project Aero 0018 ‘Euromesh’ (1990).
Kordulla, W., Schwamborn, D., Sobieczky, H.: `The DFVLR-F5 Wing Experiment - Towards the Validation of the Numerical Simulation of Transonic Viscous Wing Flows’, AGARD CP 437 “Validation of Computational Flud Dynamics”, (1988)
Rill, S., Becker, K.: `Simulation of Transonic Flow over a Twin Jet Transport Aircraft’, AIAA-91–0025, (1991)
Author information
Authors and Affiliations
Editor information
Rights and permissions
Copyright information
© 1993 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
About this chapter
Cite this chapter
Sobieczky, H. (1993). Aircraft Surface Generation. In: Weatherill, N.P., Marchant, M.J., King, D.A. (eds) Multiblock Grid Generation. Notes on Numerical Fluid Mechanics (NNFM), vol 44. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-87881-6_11
Download citation
DOI: https://doi.org/10.1007/978-3-322-87881-6_11
Publisher Name: Vieweg+Teubner Verlag
Print ISBN: 978-3-528-07644-3
Online ISBN: 978-3-322-87881-6
eBook Packages: Springer Book Archive