Axisymmetric transonic flow computations using a multigrid method

  • B. Arlinger
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 141)


AIAA Paper Multigrid Method Transonic Flow Pointed Body Supersonic Region 
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  1. Arlinger,H.,“Analysis of two-element high lift systems in transonic flow”, ICAS Paper 76-13, 1976.Google Scholar
  2. Arlinger,B.,“Multigrid technique applied to lifting transonic flow using full potential equation”, SAAB-SCANIA Rep. L-0-1 439, 1978.Google Scholar
  3. Chaussee,D.,“On the transonic flow field surrounding tangent ogive bodies with emphasis on nose drag calculations”, AIAA Paper 78-212, 1978.Google Scholar
  4. Fuchs,L.,“Finite difference methods for plane steady inviscid transonic flows”, Techn. Dr. Thesis, KTH, Stockholm, 1977.Google Scholar
  5. Hafez,M., Murman,E. and South,J.,“Artificial compressibility methods for numerical solution of transonic full potential equation”, AIAA Paper 78-1148, 1978.Google Scholar
  6. Hsieh,T.,“Unsteady transonic flow over blunt and pointed bodies of revolution”,AIAA Paper 78-211, 1978.Google Scholar
  7. Jameson,A.,“Iterative solution of transonic flows over airfoils and wings, including flows at Mach 1”, Comm. Pure Appl. Math. 27, p 283–309, 1974.Google Scholar
  8. Jameson,A.,“Acceleration of transonic potential flow calculations on arbitrary meshes by the multiple grid method”, AIAA Paper 79-1458, 1979.Google Scholar
  9. South,J. and Jameson,A.,“Relaxation solutions for inviscid axisymmetric flow over blunt or pointed bodies”, Proc. AIAA Conf. on Comp.Fluid Dynamics, Palm Springs, p B-17, 1973.Google Scholar
  10. South,J. and Brandt,A.,“Application of a multi-level grid method to transonic flow calculations”, ICASE Report Nr 76-8, Langley Research Center, 1976.Google Scholar
  11. Stanbrook,A.,“A correlation of the forebody drag of cylinders with plane and hemispherical noses at Mach numbers from zero to 2.5”, RAE TN Aero 2875, 1963.Google Scholar

Copyright information

© Springer-Verlag 1981

Authors and Affiliations

  • B. Arlinger
    • 1
  1. 1.SAAB-SCANIA ABLinköpingSweden

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