Summary
The aerodynamics of combustion chambers for aeronautical engines is studied by means of a compressible Navier-Stokes solver without chemical reactions. The three-dimensional (3-D) code is designed for the simulation of complex geometries by introducing non orthogonal curvilinear coordinates. The implicit solver, which is based on the scalar approximate factorization method, accounts for turbulence effects by using a zero-equation turbulence model and solves in terms of primitive variables. Particular care is devoted to boundary conditions to account properly for swirl velocities and cooling air lateral holes. The code showed good flexibility and design capability for 3-D complex flow fields. The tests show that the presence of circumferential and toroidal recirculation zones can be controlled by either the inlet swirl velocity or the lateral jet holes.
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References
Wassel, A.B., “Combustion Problems in Gas Turbine Applications: The Design and Development of High Performance Combustore”, Von Karman Institute for Fluid Dynamics, January 10–14 1977.
McGuirk, J.J., J.M. Palma, “The Flow Inside a Model Gas Turbine Combustori Calculations”, Transaction of the ASME, Vol. 115, July 1993.
Ahmed, S.A., Nejad, A.S., “Swirl Effects on Confined Flows in Axisymmetric Geometries”, Journal of Propulsion and Power, Vol.8, No. 2, March-April 1992.
Escudier, M.P., Keller, J.J., “Recirculation in Swirling Flow: A Manifestation of Vortex Breakdown”, AIAA JOURNAL, Vol. 23, No. 1, January 1985.
Benjamin, T.B., “Significance of the Vortex Breakdown Phenomenon”, Transaction of the ASME, June 1965.
Michelassi, V., Liou, M.-S., Povinelli, L.A., Martelli, F., 1990, “Implicit Solution of Three-Dimensional Internal Turbulent Flows”, NASA CP-10045.
Michelassi, V., Martelli, F., 1993, “3-D Implicit Navier-Stokes Solver for Internal Turbulent Compressible Flows”, Journal de Phys. III, France 3, pp. 223–235.
Pulliam, T.H., Chaussee, D.S., 1981, “A Diagonal Form of an Implicit Approximate-Factorization Algorithm”. Journal of Computational Physics, N. 39.
Jameson, A., Schmidt, W., Türkei, E., 1981: “Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes”, AIAA 81-1259.
Michelassi, V., Theodoridis, G.S., Papanicolaou, E.L., “Low Speed Turbine Computation by Pressure-Correction and Time-Marching Methods”, Proceedings, ASME 1995 International Mechanical Engineering Congress & Exposition (IMECHE), 12–17 November 1995, San Francisco (CA), USA.
Benelli, G., Private Communication, ENEL-Italy, 1994.
Hogg, S., Leschziner, M.A., “Computation of Highly Swirling Confined Flow with a Reynolds Stress Turbulence Model”, AIAA JOURNAL, Vol. 27, No. 1, January 1989.
Fu, S., Huang, P.G., Launder, B.E., Leschziner, M.A., “A Comparison of Algebraic and Differential Second-Moment Closures for Axiaimmetric Turbulent Shear Flows Whith and Without Swirl”, Transaction of the ASME, Vol. 110, June 1988.
Baldwin, B.S., Lomax, H., “Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows”, AIAA 16TH AEROSPACE SCIENCES MEETING Huntsville, Alabama January 16–18, 1978.
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© 1996 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
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Michelassi, V., Martelli, F., Pigari, F. (1996). Aerodynamics of Combustion Chambers for Aeronautical Engines. In: Deville, M., Gavrilakis, S., Ryhming, I.L. (eds) Computation of Three-Dimensional Complex Flows. Notes on Numerical Fluid Mechanics (NNFM), vol 49. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-89838-8_22
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DOI: https://doi.org/10.1007/978-3-322-89838-8_22
Publisher Name: Vieweg+Teubner Verlag
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