Skip to main content
SpringerLink
Log in

Geometry Generator for CFD and Applied Aerodynamics

  • Chapter
New Design Concepts for High Speed Air Transport

Part of the book series: International Centre for Mechanical Sciences ((CISM,volume 366))

Abstract

This chapter is intended to combine the knowledge bases of applied geometry with those of hydrodynamics and aerodynamics, including the modest additions presented in the two previous book chapters focusing on the interaction between compressible flow with shock waves and flow boundary conditions. The need to have flexible tools for effectively influencing the phenomena occurring in high speed flow calls for development of fast and flexible software to create shapes in a way to have easy access to the crucial shape-generating parameters controlling these flow phenomena, and at the same time observe the constraints given by structural and other practical limitations.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Log in via an institution
Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 39.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 54.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. 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

    Google Scholar 

  2. Pagendarm, H. G., Laurien, E., Sobieczky, H. Interactive Geometry Definition and Grid Generation for Applied Aerodynamics. AIAA 88–2415CP, 1988

    Google Scholar 

  3. Sobieczky, H., Stroeve, J. C. Generic Supersonic and Hypersonic Configurations. AIAA 91–3301CP, 1991

    Google Scholar 

  4. Sobieczky, H. DLR-F5: Test Wing for CFD and Applied Aerodynamics, Case B-5 in: Test Cases for CFD Evaluation. AGARD FDP AR-303, 1994

    Google Scholar 

  5. Pagendarm, H. G.: Unsteady Phenomena, Hypersonic Flows and Co-operative Flow Visualization in Aerospace Research. In: G.M. Nielson, D. Bergeron, (Eds), Proceedings Visualization `93, pp. 370–373, IEEE Computer Society Press, Los Alamitos, CA, 1993

    Google Scholar 

  6. Cosentino, G. B., Holst, T. L. Numerical Optimization Design of Advanced Transonic Wing Configurations. Journal of Aircraft, Vol. 23, pp. 192–199, 1986

    Google Scholar 

  7. Hannemann, M., Sobieczky, H. Visualization of High Speed Aerodynamic Configuration Design. In: G. M. Nielsen, D. Silver, Proc. Visualization `95, pp. 355–358, IEEE Computer Society Press, Los Alamitos, CA, 1995

    Google Scholar 

  8. Zhu, Y., Sobieczky, H. Numerical Optimization Method for Transonic Wing Design. Proc. 6th Asian Congress of Fluid Mechanics, Singapore, 1995

    Google Scholar 

  9. Sobieczky, H., Seebass, A. R. Adaptive Airfoils and Wings for Efficient Transonic Flight. ICAS paper 80–11.2, 1980

    Google Scholar 

  10. Geissler, W., Sobieczky, H. Unsteady Flow Control on Rotor Airfoils. AIAA 95–1890, 1995

    Google Scholar 

  11. Kulfan, R. High Speed Civil Transport Opportunities, Challenges and Technology Needs. Lecture at Taiwan IAA 34th National Conference, 1992

    Google Scholar 

  12. Kroll, N., Radespiel, R. An Improved Flux Vector Split Discretization Scheme for Viscous Flows. DLR-FB 9353, 1993

    Google Scholar 

  13. Pagendarm, H. G., Choudhry, S. I. Visualization of Hypersonic Flows - Exploring the Opportunities to Extend AVS, 4th Eurographics Workshop on Visualization in Scientific Computing, 1993

    Google Scholar 

  14. Becker, K., Rill, S. Multiblock Mesh Generation of Complete Aircraft Configurations. In: N. P. Weatherill, M. J. Marchant, D. A. King (Eds), Multiblock Grid Generation Results of the EC/ BRITE-EURAM EUROMESH, 1990–92. Notes on Numerical Fluid Mechanics, Vol. 44, pp. 130–138, Braunschweig; Wiesbaden: Vieweg, 1993

    Google Scholar 

  15. Orlowsky, M., Herrmann, U. Aerodynamic Optimization of Supersonic Transport Configurations. Proc. 20th International Council of the Aeronautical Sciences Congress, ICAS 96.4.4.3, 1996

    Google Scholar 

  16. Trapp, J., Zores, R., Gerhold, Th., Sobieczky, H. Geometrische Werkzeuge zur Auslegung Adaptiver Aerodynamischer Komponenten. Proc. DGLR Jahrestagung `96, Dresden, 1996

    Google Scholar 

  17. Gerhold, Th., Friedrich, O., Galle, M. Calculation of Complex Three-Dimensional Configurations Employing the DLR-TauCode. AIAA 97–0167, 1997

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. DLR German Aerospace Research Establishment, Gottingen, Germany

    H. Sobieczky

Authors
  1. H. Sobieczky
    View author publications

    You can also search for this author in PubMed Google Scholar

Editor information

Editors and Affiliations

  1. DLR German Aerospace Research Establishment, Germany

    H. Sobieczky

Rights and permissions

Reprints and permissions

Copyright information

© 1997 Springer-Verlag Wien

About this chapter

Cite this chapter

Sobieczky, H. (1997). Geometry Generator for CFD and Applied Aerodynamics. In: Sobieczky, H. (eds) New Design Concepts for High Speed Air Transport. International Centre for Mechanical Sciences, vol 366. Springer, Vienna. https://doi.org/10.1007/978-3-7091-2658-5_9

Download citation

  • DOI: https://doi.org/10.1007/978-3-7091-2658-5_9

  • Publisher Name: Springer, Vienna

  • Print ISBN: 978-3-211-82815-1

  • Online ISBN: 978-3-7091-2658-5

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics

Search

Navigation