Predicting Unsteady Flow Parameters in a Subsonic Air Diffuser Using MacCormack’s Explicit Method
DOI:
https://doi.org/10.31185/ejuow.Vol7.Iss1.109Keywords:
Subsonic flow, CFD, Fluid mechanicsAbstract
A numerical procedure is presented to predict the flow characteristics inside a subsonic diffuser by solving Navier-Stokes' equations, using MacCormack’s explicit method. The flow is assumed to be viscous, compressible, unsteady and two-dimensional. The grid model suggested for the diffuser has 20 points in the horizontal direction and 30 points in the vertical direction. The numerical solution has shown reasonable results with a 2D variation of flow properties inside the diffuser and the steady state solution can be satisfied by 600-900 loops only. The obtained results of the present study are compared with those obtained by using a numerical code of National Project for Application-oriented Research in CFD (NPARC) as well as those obtained from a previous experimental study and give an acceptable range of errors (about ± 15%).
References
[2] Abboudi S., Deng J. and Imbert M., 2007, “Thermal Wall Influence on the Behavior of Axisymmetric Laminar Compressible Flow in Nozzle”, Journal of Computational and Applied Mechanics, Vol. 8, No. 1, Pages 5–19
[3] Pardyjak E., "Introduction to Compressible Flow", Notes of Mechanical Engineering Department, University of Utah, www.mech.utah.edu, Accessed on 24/2/2016
[4] Pauls W., 2010, “On Complex Singularities of the 2D Euler Equation at Short Times”, Physica D 239, Pages 1159-1169, Elsevier Science Publishing Company
[5] Swisshelm M., Johnson G. and Kumar S., 1986. “Parallel Computation of Euler and Navier-Stokes Flows, Applied Mathematics and Computation Vol. 19, Pages 321-331, Elsevier Science Publishing Company
[6] Dudek, J.C., N. J. Georgiadis, and D. A. Yoder, 1996, "Calculation of Turbulent Subsonic Diffuser Flows Using the NPARC Navier-Stokes Code", NASA TM, AIAA Paper 96-0497
[7] Abbood A.H., 1999, "Numerical Analysis of Two-Dimensional Convergent-Divergent Nozzle for A Modern Fighter". MSc. Thesis, College of Military Engineering, Baghdad
[8] Rosello M., 2002, “Analytic-Numerical Approach to Flow Calculation in Intake and Exhaust Systems of Internal Combustion Engines”, Mathematical and Computer Modelling, Vol. 36, Pages 33-45
[9] Jalal M. Jalil and Ahmed F. Kridy, 2009, “Numerical Simulation of a Two-Dimension Ramp Inlet Flow Field”, Engineering and Technology Journal, Vol. 27, No. 6, Pages 1117-1124
[10] Sinha P., A.N. Mullick, B. Halder and B. Majumdar, 2011, "Numerical Investigation of Performance Characteristics in Annular Subsonic Diffuser", IJRMET Vol. 1, Issue 1, pages 79-83, Oct. 2011
[11] Berens M., 2015, "Numerical and Experimental Investigations on Subsonic Air Intakes with Serpentine Ducts for UAV Configurations", 5th Air and Space Conference, CEAS, Paper No. 074, 2015
[12] Anderson D.A., J.C. Tannehill, and R.H. Pletcher, 1984, "Computational Fluid Mechanics and Heat Transfer", McGraw-Hill Company
[13] Patrick H. Oosthuizen and William E.Carscallen, 1997, "Compressible Fluid Flow", McGraw-Hill Company
[14] Driver D. M., and Johnson J. P., "Experimental Study of a Three-Dimensional Shear-Driver Turbulent Boundary Layer with Streamwise Adverse Pressure Gradient", NASA TM 102211, May 1990