3D Euler Flows Around Modern Airplanes

  • J. L. Kuyvenhoven
  • J. W. Boerstoel
Conference paper
Part of the Notes on Numerical Fluid Mechanics (NNFM) book series (NNFM, volume 29)


The numerical simulation of flows around complex aircraft configurations like the Fokker 50 and Fokker 100, is described. In these simulations multiblock grids and a 3D Euler-flow solver are used.

The major features of the grid-generation procedure and flow solver are outlined.

Results of the validation of the numerical-flow-simulation system for aerodynamic design work are presented.


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  1. [1]
    Voogt, N., Mol, W.J.A., Stout. J., and Volkers, D.F.: “CFD applications in design and analysis of the Fokker 50 and Fokker 100”, AGARD conference, Lisbon, Portugal (1988), pp 19-1 to 19-11.Google Scholar
  2. [2]
    Boerstoel, J.W.: “Numerical grid generation in 3D Euler flow simulation”, in: Numerical methods for Fluid Dynamics, Ed. Morton, K.W., Baines, M.J. Clarendon Press, Oxford (1988).Google Scholar
  3. [3]
    Allwright, S.: “Multiblock topology specification and grid generation for complete aircraft configurations”, AGARD specialists’ meeting, 24-25 May 1989, Norway.Google Scholar
  4. [4]
    Thompson, J.F., Thames, F.C., Mastin, C.W.:. “Automatic Numerical Generation of Body-Fitted Curvilinear Coordinate System for Field Containing any Number of Arbitrary Two Dimensional Bodies”, J. Comp. Phys. 15, 1974.Google Scholar
  5. [5]
    Boerstoel, J.W.: “Problem and solution formulations for the generation of 3D block-structured grids”, NLR MP 86020U (1986).Google Scholar
  6. [6]
    Jacobs, J.M.J.W. et al.: “Numerical interactive grid generation for 3D flow calculations”, in: Numerical grid generation in computational fluid dynamics 88, Ed. Sengupta, S., Peneridge Press (1988).Google Scholar
  7. [7]
    Jameson, A., Schmidt, W., Turkel, E.: “Numerical solution of Euler equations by finite volume methods using Runge Kutta time stepping schemes”, AIM paper 81-1259.Google Scholar
  8. [8]
    Amendola, A., Tognaccini, R., Boerstoel, J.W. and Kassies, A.: “Validation of a multiblock Euler flow solver with propeller-slipstream flows”, AGARD conference proceedings, Lisbon, Portugal (1988), pp P1-1 to P1-15.Google Scholar
  9. [9]
    Kuyvenhoven, J.L.: “3D Euler calculations about the Fokker 100”, Fokker report L-28-459, 1988.Google Scholar

Copyright information

© Springer Fachmedien Wiesbaden 1990

Authors and Affiliations

  • J. L. Kuyvenhoven
    • 1
  • J. W. Boerstoel
    • 2
  1. 1.Fokker Aircraft B.V.Schiphol-OostThe Netherlands
  2. 2.National Aerospace Laboratory NLRAmsterdamThe Netherlands

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