Скачать 46.23 Kb.
Размер46.23 Kb.



[1] Barnard, R. H, and D. R. Philpott, “ Aircraft Flight”, Longman Scientific and Technical, P.28 (1989).

[2] Courant, R.,Isaacson, E., and Reeves, M. “On the Solution of Nonlinear Hyperbolic Differential Equations By Finite Differences”, Comm. Pure and Applied Mathematics, Vol. 5, P.P. 243-255, (1952).

[3] Mohammad Mostafa Gogze, “Three diemension turbulent Flow Prediction Between Two Axial Compressor Blades Using Body Fitted Coordinate system”, P.hd thesis, Mech. Engineering department, Baghdad university June (2000)

[4] Fletcher, C.A.J. “Computational Techniques for Fluid Dynamics 2, Springer Series in J. of Computational Physics, Second Edition, Springer-Verlag Berlin Heidelberg, P.P.46-200, Germany,(1991).

[5] Thompson, J.F., Thames, F.C., and Mastin C.W., “Automatic Numerical Generation of Body Fitted Curvilinear Coordinate System for field Containing any Number of Arbitrary Two-Dimensional Bodies”, J. of Computational Physics, Vol. 15, P.P. 299-319 (1974).

[6] Joseph L. Steger, “Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimension Geometries”, AIAA J. Vol. 16, July(1978).

[7] Condunov, S. K. and Prokopov, G. p., The Use of Moving Meshes in Gas Dynamics Computations”, J. of Computational Physics, Vol. 15, P.P 299-319(1974).

[8] Barfield, W.D., “An Optimal Mesh Generator for Lagrangian Hydrodynamics Calculations in Two Space Dimensions” ,J. of Computational Physics, Vol 6, P.P 417-420 (1970).

[9] Visbal M.,Knight D., “Generation of Orthogonal and Nearly Orthogonal Coordinates with Grid Control Near Boundaries”, AIAA. J., Vol 20, No.3 , March (1982).

[10] Thomas, P.D. and Middlecoff, J.F. “Direct Control of the Grid Point Distribution in Meshes Generated by Elliptic Equations” AIAA. J., Vol.18, P.P. 652-657(1980).

[11] “ Analysis of Fluid- Structure Interaction on Moving Airfoils by means of Dynamic Instructed Meshes”, Proceedings of 4th international Symposium of Fluid-Structure, vol. I ASME, (2002)

[12] Steger, J. L. and chaussee, D. S., “Generation of Body Fitted Coordinates Using Hyperbolic Partial Differential Equations”, SIAM J. Vol.1, P.P.431-437, Dec.(1980).

[13] Nakamura,S., “Non-Iterative Grid Generation Using Parabolic Differential Equations of Fuselage-Wing Flow Calculations”, Eighteen International Conference on Numerical(1980)..

[14] Haussling and Coleman “A Method for Generation of Orthogonal and Nearly Orthogonal Boundary Fitted Coordiants Systems”, J. of Computational Physics, Vol. 43 , P.P. 373-381,(1981).

[15] Papantonis, D.E, and Athanassiadis N.A. “A Numerical Procedure for the Generation of Orthogonal Body Fitted Coordinate Systems With Direct Determination of Grid Points on the Boundary”, International J. for Numerical Methods in Fluids, Vol.5, P.P.245-255 (1985).

[16] Thames, F.C., Thompson, J.F., Mastin, C.W. and Walker R.L. “Numerical Solutions for viscous and Potential Flow about Arbitrary Two-Dimension Bodies Using Body-Fitted Coordinate System”, J. of Computational Physics, Vol.24, p.p. 245-273,(1977).

[17] Galpin, P.F.,Doormaal,J.P.V., and Raithby, G.D., “Solution of the incompressible Mass and Momentum Equations by Application of a coupled Equation line Solver” International J. for Numerical Methods in Fluids, Vol. 5, P.P. 615-625 (1985).

[18] Patel, M.K., Markatos, N.C.,Gross,M., “A Critical Evaluation of Seven Discretization Schemes for Convection-Diffusion Equations”, International J. for Numerical Methods in Fluids, Vol.5 P.P 255-244 (1985) .

[19] Ferreri, J.C. and Ventura, M.A. “On the Accuracy of Boundary Fitted Finite Difference Calculations”, International J. for Numerical Methods in Fluids, Vol.. 4, P.P. 359-375, (1984).

[20] Gresho, P.M. and Sani, R.L. “On Pressure Boundary Conditions for the Incompressible Navier Stokes Equations” International J. for Numerical Methods in Fluids, Vol. 7, P.P 1111-1145, (1987).

[21] Rodi, W.M. and Schonung, B., “Finite Volume Method for Two Dimensional Incompressible Flow with Complex Boundaries” Coputer Method in Applied Mechanics and Eng., Vol. 75, P.P. 369-392, (1989).

[22] Kumar, K.R., Rankin, G.W. and Sridhar, K. “Fully Developed Flow of Power Law Fluids in Curved Ducts with Heat Transfer”, Numerical Heat Transfer, Part A., Vol. 16, P.P. 101-118,(1089).

[23] Chima, V.R. and Yokota, J.W. “Numerical Analysis of Three Dimensional Viscous Internal Flow” AIAA. J. , Vol. 28, No. 5,P.P.798-806, May(1990)..

[24] Kunz, R.F., Rhie, C.M. and Malelecki, R.E. “Calculation of Internal Flow Using Single Pass Parabolized Navier Stockes Analysis”, AIAA. J., Vol.28, No.5, (1990).

[25] Essers, J.A., Delanaye, M. and Rogiest, P. “Upwind Based Finite Volume Technique Solving Navier Stokes Equations on Irregular Meshes”, AIAA. J., Vol.33, No. 5, P.P. 833-842 May(1995).

[26] Saxena, S.K. and Ravi, K. “Some Aspects of High Speed Flow Computations with Roe Scheme”, AIAA. J., Vol.33, No. 6, P.P. June(1995).

[27] Lax, P.D. “Hyperbolic System of Conservation Law II” Comm. Pure and Applied Mathematics, Vol. 10, P.P. 537-566, (1957).

[28] Lax, P.D. and Wendroff, B., “System of Conservation Law II”, Computer and Applied Mathematics, Vol. 13, P.P. 217-237 (1960).

[29] S. M. Han, S. T. Wu . and M. Dryer, “A three-Dimension , Time-Dependent Numerical Modeling of Supersonic Super-Alfenic MHD Flow”, J. of Computer and Fluids, Vol. 16 No. 1, P.P. 81-103,(1988).

[30] MacCormak, R. W. “The Effect of Viscosity on Hypervelocity Impact Creating,” AIAA. Hyper. Velocity Impact Conference, Paper 69 –354,(1969).

[31] Migdal, D., Klein K. and Moretti G., Time Dependent Calculation for Transonic Nozzle Flow”, AIAA. J., Vol.7, P.P.449-457, (1981).

[32] Anderson, John D. Jr., “ A Time Dependent Analysis for Vibration and Chemical Non equilibrium Nozzle Flows”, AIAA. J., Vol. 8, P.P. 545-550, (1970).

[33] Serra, R. A., “The Determination of Internal Gas Flows by a Transient Numerical Technique”, AIAA. J. Vol. 10, P.P.603-611, May(1972).

[34] Denanly, R. A. and Kavanagh, P. “ Transonic Flow Analysis in Axial Flow Turubomachinary Cascades by a Time Dependent Method of Characteristics”, J. of Engineering for Power, P.P. 356-364, July (1976).

[35] Moretti, G., “The -Scheme”, Computer and Fluids, Vol.17 P.P. 191-205(1979).

[36] Steger, J. L., and Warming R.F. “Flux Vector Splitting of the Inviscid as Dynamic Equations with Application of Finite Difference Methods.” ,J. of Computational Physics, Vol 40, P.P 263-293 (1981).

[37] Van Ler, B. “ Flux Vector Splitting for the Euler Equation”, in Proc. 8th International conference on Numerical Methods in fluid dynamics, Springer, Verlag, (1982).

[38] Boris, J.P. Book, D. I. “Flux Corrected Transport I. Shasta, A Fluid Transport Algorithm That Work ”,J. of Computational Physics, Vol. 2,, P.P 38-69 (1973).

[39] Stile, R. J. and Hoffman, J .D., “Analysis of Steady Two-Dimensional Chemically reacting, Non Equilibrium inviscid Flow in Nozzles”, AIAA, J. Vol. 23, P.P. 242-348, March(1985).

[40] Rodrick V. Chima and Gary M. Johnson, “Efficient Solution of the Euler and Navier-Stokes Equations with a Vectorized Multiple-Grid Algorithm”, AIAA J. Vol. 23 No. 1, (1985).

[41] Scott L. Lawrence and J. C. Tannehill and Denny S. Chaussee, “ Application of the Implicit MacCormak Scheme to the Paraboliized Navier-Stokes Equations”, AIAA J. Vol.22, No. 12, Dec.(1984).

[42] http: web pages “Solution Technique” (2002).

[43] Versteeg, H. K. and Malalasekera,, “An Introduction to Computational Fluid Dynamic, the Finite Volume Method”, Longman Scientific and Technical, (1995).

[44] Klaus A. Hoffmann, Computational Fluid Dynamics for Engineers” (1989).

[45] Baldwin, B. S. and Lomax H., “ Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows,” AIAA. Paper 78-0257, (1978).

[46] Cebeci, T., and Smith, AM. O “Analysis of Turbulent Boundary Layers”, New York, Academic Press.(1974).

[47] Siamack A. Shirazi and C. Randall Truman, “ Evaluation of Algebraic Turbulence Models for PNS Predications of Supersonic Flow Past a Sphere-Cone”, AIAA J., Vol. 27 , No 5 (1988).

[48] F. M. Al-Dulaimy “ Numerical of Supersonic Inviscid and Viscose Flow Over Arbitrary Configuration”, P.H.D. Thesis, Jan.(2002).

[49] Leschziner, M. A. and Rodi, W. “Calculation of Annular and Twin Parallel Jets Using Various Discrctization Shemes and Turbulence Model Variation”, ASME. J., Of Fluid Eng., Vol. 103, P.P. 252-360,(1981).

[50] Y. Wang and S. Komori, “ Simulation of the Subsonic Flow in a High-Speed Centrifugal Compressor Impeller by the Pressure-Based Method”, Proc. Instn. Mech. Engrs. Vol.212 Part A , (1998).

[51] Lunder, B.E. and Spalding, D.B., “ The Numerical computation of Turbulent Flows”, Computer Methods in Applied Mechanics and Engineering, Vol. 3, P.P. 269-289 , (1974).

[52] Thomas H. Pulliam, “ Artificial Dissipation Models for The Euler Equations”, AiAA. J., Vol.24, No. 12, Dec. (1986).

[53] Roe , P.L, “ The Use of the Riemann Problem in Finite Difference Schemes”, Fluid Dynamic J., (1980).

[54] Van Leer, B., “ Flux- Vector Splitting for the Euler Equation”, Fluid Dynamic J. Vol. 12 (1983).

[55] Osher, S. and Chakravarthy, S., “ upwind scheme and Boundary Condition With Application to Euler Equation in General Geometries ”, J. of Computational Physics, Vol. %0 P.P. 447-481, (1983).

[56] G. Q. Chen, “Shock Capturing and Related Numerical Methods in Computational Fluid Dynamics”, Proceedings of Algoritmy (2000).

[57] Anderson, John D., Jr., “Computational Fluid Dynamic, the Basic with Application”, McGraw- Hill, New York, (1995).

[58] Anderson, J. D., “Fundamental of Aerodynamics”, 2nd Edition, McGraw-Hill, (1991).

[59] Oktay Baysal, “Super Computing of Supersonic Flows using Upwind Relaxation and MacCormak Schemes”, Transactions of the ASME, Vol.110, March (1988).

[60] C.M. Rhie, “A Three-Dimensional Passage Flow Analysis Method Aimed At Centrifugal Impellers”, J. for Computers and Fluid, Vol.13 No.4, P.P.443-460, (1985).

[61] Z. Petrovic and S. Stupar, “CFD One Computational Fluid Dynamics One”, Mechanical Engineering Facuity Belgrade, (1996).

[62] P.D.Thomas and J. F. Middlecoff, “ Direct Control of the Grid Points Distribution in Meshes Generated by Elliptic Equation”, AIAA. J. Vol. 18, No. 6 , (1979).

[63] htt: // ww.ode-wep. Demo. /flucome / titles.html, “ Study on Three Dimensional Vertical Structure on the Flow Around Circular Cylinder”, Flucome Papers and Short Abstracts Received @ 24th July (2003).

[64] O. Baysal and K. Fouladi and D.S. Miller, “Computational of Supersonic Flows Over a Body at High Angle of Attack” AIAA J. Vol. 27, No. 4 ,April (1989).

[65] Lin, T. C., Reeves, B. L., and Siegelaman, “ Blunt- Body Problem in Non uniform Flow Fields”, AIAA. J, Vol. 15,, P.P. 457-470, Aug.(1977).

[66] Childress, s., “ Solution of Eulers Equations Containing Finite Eddies”, Physics of Fluids, Vol. 9, P.P. 860-872, May (1986).

[67] Ajay Kumar, and M. D. Salas, “ Euler and Navier Stocks Solution for Supersonic Shear Flow Past a Circular Cyliunder”, AIAA. J., Vol.23, No.4, April(1985).

[68] Jack Moran, “An Introduction to Theoretical and Computational Aerodynamics”, (1984).

[69] M.Kenan, “Ceramic Bulletin”, Vol. 69, No. 5, (1990).

[70] Bahjat Bahloul Kahdim , “Study of Friction, Wear and Electrical Resistivity of Graphite DMMA/PS Composites”, B. Sc. University of Baghdad , Jan(2000).

[71] N. J. Welham, and J. S. Williams, “ Extended Milling of Graphite and Activate Carbon”, Carbon J. Vol. 36, No. 9, P.P. 1309-1315, (1998).

[72] Chemical hand book “ Plastic”, Dec.(1982).

علي لفتة “دراسة عددية لأنتقال الحرارة بالحمل القسري خلال مجموعة من[73] الانابيب بأستخدام نظام مطابقة أحداثيات الجسم " أطروحة ماجستير مقدمة لقسم المكائن والمعدات في الجامعة التكنلوجية, (2002).


References iconNote: This bibliography includes both references cited and references useful for background information

References iconNote: This bibliography includes both references cited and references useful for background information

References iconReferences References

References iconReferences

References iconReferences

References iconReferences

References iconReferences

References iconReferences

References iconReferences

References iconReferences

Разместите кнопку на своём сайте:

База данных защищена авторским правом © 2014
обратиться к администрации
Главная страница