Skip to main content

Use of CFD and Experiment in Transonic Aircraft Design

  • Conference paper

Abstract

The aerodynamic design of an aircraft involves the total flight envelope — flight ranging from takeoff and landing at low speeds to cruise at transonic Mach numbers, and to flight at the maximums speeds, Mach numbers, angles of attack and yaw that the aircraft will forseeably encounter. The design issues, the parameters of interest, and the dominant fluid physics can be vastly different for these different regimes of flight.

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

Buying options

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   84.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   109.99
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

Learn about institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Tinoco, E. N., “Transonic CFD Applications at Boeing,” Presented at the Transonic Symposium, NASA Langley Research Center, Hampton, VA., April 19–21, 1988

    Google Scholar 

  2. Snepp, D. K. and Pomeroy, R. C., “A Geometry System for Aerodynamic Design,” AIAA Paper 87–2902, September, 1987.

    Google Scholar 

  3. Buning, P. G. and Steger, J. L., “Graphics and Flow Visualization in Computational Fluid Dynamics,” AIAA Paper 85–1507-CP, July, 1985

    Google Scholar 

  4. Rubbert, P. E., “Design Applications of CFD at Boeing,” Presented at the NAS Dedication, NASA Ames Research Center, November, 1986.

    Google Scholar 

  5. Bengelink, R. L., “The Use of Computational Fluid Dynamics in Predicting Full Scale Aircraft Aerodynamics,” Presented at the International Symposium on Aeronautical Science and Technology (ISASTI 86 ), Jakarta, Indonesia, June 1986

    Google Scholar 

  6. Rubbert, P. E. and Tinoco, E. N., “Impact of Computational Methods on Aircraft Design” (Invited Paper), AIAA Paper 83–2060, August, 1983.

    Google Scholar 

  7. Yu, N. J., Kusunose, K., Chen, H. C., and Sommerfield, D. M., “Flow Simulations for an Aft-Mounted Propfan Using Euler Equations,” SAE Technical Paper 861718, Long Beach, CA, October, 1986.

    Book  Google Scholar 

  8. Tinoco, E. N., Ball, D. N., and Rice II, F. A., “PAN AIR Analysis of a Transport High-Lift Configuration,” Journal of Aircraft, Vol. 24, No. 3, March, 1987.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 1989 Springer-Verlag Berlin Heidelberg

About this paper

Cite this paper

Rubbert, P. (1989). Use of CFD and Experiment in Transonic Aircraft Design. In: Zierep, J., Oertel, H. (eds) Symposium Transsonicum III. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-83584-1_2

Download citation

  • DOI: https://doi.org/10.1007/978-3-642-83584-1_2

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-83586-5

  • Online ISBN: 978-3-642-83584-1

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics