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Viscous transonic airfoil flow simulation

Wybrane pełne teksty z tego czasopisma
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
A calculation method for the subsonic and transonic viscous flow over airfoil using the displacement surface concept is described. This modelling technique uses a finite volume method for the time-dependent Euler equations and laminar and turbulent boundary-layer integral methods. Additionally special models for transition, laminar or turbulent separation bubbles and trailing edge treatment have been selected. However, the flow is limited to small parts of trailing edge-type separation. Comparisons with experimental data and other methods are shown.
Rocznik
Strony
687--699
Opis fizyczny
Bibliogr. 21 poz., wykr.
Twórcy
  • Institute of Statistics and Applied Mathematics 13 September Street, Sect. V, Bucharest, ROMANIA
  • Department of Aerospace Engineering, University "POLITEHNICA" of Bucharest 1 Gh. Polizu Street, Sect.1, ROMANIA
Bibliografia
  • [1] van Albada, van Leer B. and Roberts W.W. (1982): A comparative study of computational methods in cosmic gas dynamics. - Astron. Astrophysics, vol. 108, pp.76-84.
  • [2] Cebeci T. (1999): An Engineering Approach to the Calculation of Aerodynamic Flows. - Springer-Verlag.
  • [3] Coiro D.P., Amato M. and De Matteis P. (1992): Numerical predictions of transonic viscous flows around airfoils through an Euler/boundary layer interaction method. - Aeronautical Journal, April, pp. 157-165.
  • [4] Cook P.H., McDonald M.A. and Formin M.C.P. (1979): Aerofoil RAE 2822 Pressure Distribution and Boundary Layer and Wake Measurements. Experimental Data Base for Computer Program Assessment. - AGARD Report AR-138/1979.
  • [5] Drela M. and Giles B.B. (1987): Viscous-inviscid analysis of transonic and low Reynolds number airfoils. - AIAA Journal, vol.25, pp. 1347-1355.
  • [6] Goradia S.H. and Lyman V. (1974): Laminar stall prediction and estimation of CL max. - Journal of Aircraft, vol.11, pp.528-536.
  • [7] Hirsch C.A. (1990): Numerical Computation of Internal and External Flows. - Wiley and Sons.
  • [8] Holst T.L., Kaynak U. And Grundy K.L. (1987): Transonic wing flows using an Euler/Navier-Stokes zonal approach. - Journal of Aircraft, vol.24, No. 1, ppl7-24.
  • [9] Horton H.P. (1967): Laminar Separation Bubbles in Two and Three Dimensional Incompressible Flow. - Ph.D. Thesis, Queen Mary College, University of London.
  • [10] Horton H.P. (1969): Entrainment in Equilibrium and Non-equilibrium Turbulent Boundary Layers. - Rep. Research/1094/HPH, Hawker Siddeley Aviation Ltd., Hartfield.
  • [11] Jameson A., Pierce N.A. and Martinelli (1997): Optimum aerodynamic design using the Navier-Stokes equations. - AIAA, Paper No.97-0101, January, pp.1-22.
  • [12] Jameson A., Turkel E. and Schmidt W. (1981): Numerical Simulation of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-steping Schemes. - AIAA, Paper No.81-1259, AIAA 14th Fluid and Plasma Dynamic Conference, Palo Alto, June, 1981, pp.1-17.
  • [13] Jayaram M. and Jameson A. (1988): Multigrid solution of Navier-Stokes equations for flow over wings. - AIAA, Paper No.88-0705, AIAA 26th Aerospace Sciences Meeting, Reno, January, 1988.
  • [14] Leicher S. (1980): Viscous flow simulation on high lift devices at subsonic and transonic speed. - AGARD Conf. Proc. 291, pp.6.1-6.15.
  • [15] Lock R.C. and Williams B.R. (1987): Viscous-inviscid interactions in external aerodynamics. - Progress Aerospace Sciences, vol.24, pp. 151-171.
  • [16] Mavriplis D. and Jameson A. (1990): Multigrid solution of the Navier-Stokes equations on triangular meshes. - AIAA Journal, vol.28, pp. 1415-1425.
  • [17] Melnik R.E., Chow R.R., Mead H.R. and Jameson A. (1985): An Inproved Viscid/inviscid Interaction Procedure for Transonic Flow over Airfoils. - NASA CR-3805 Report, October 1985.
  • [18] Roe P.L. (1981): Approximated Riemann solvers. Parameter vectors and difference scheme. - Journal of Computational Physics, vol.43, pp.357-372.
  • [19] Schmidt W., Jameson A. and Whitfield D.D. (1981): Finite volume solutions for the Euler equations for transonic flow over airfoils and wings including viscous effects. - AIAA, Paper No.81-1265, June, 1981 (J. Aircraft, vol.20, 1983, pp. 127-133).
  • [20] Squire H.B. and Young B.A. (1938): The Calculation of Profile Drag of Airfoils. - R&M No.1838/1937, British A.R.C. 1938.
  • [21] Zienkiewicz O.C. and Taylor R.L (1989): The Finite Element Method. - New York: McGraw-Hill, 4-th Ed., vol.l and 2.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BPZ2-0007-0044
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