Numerical modeling requirements for coaxial and chevron nozzle flows

9th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2003, Pages

  Birch, Stanley F ^a   Lyubimov, D A ^b   Secundov, A N ^b   Yakubovsky, K Ya ^b  

^a BOEING COMPANY   (United States)

^b Scientific and Research Center ECOLEN   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; NOZZLES; TURBULENCE MODELS;

AXISYMMETRIC GEOMETRIES; AXISYMMETRIC JET; CFD CODES; CHEVRON NOZZLE; COAXIAL-JET FLOWS; MODEL MODIFICATION; MODEL REQUIREMENTS; ZONAL MODEL;

COMPUTATIONAL FLUID DYNAMICS;

EID: 85099775709     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3287     Document Type: Conference Paper

References (25)

1. Kenzakowski, D. C., Shipman, J., Dash, S. M., Bridges, J. E. and Saiyed, N. H., "Turbulence Model Study of Laboratory Jets with Mixing Enhancements for Noise Reduction," AIAA-2000-0219.
2. Bridges, J. E., "Measurements of Turbulent Flow Field in Separate Flow Nozzle With Enhanced Mixing Devices - Test Report," NASA/TM-2002-211366.
3. Koch, L. D., Bridges, J. E., Khavaran A., "Flowfield Comparisons From Three Navier- Stokes Solvers for an Axisymmetric Separate Flow Jet," AIAA-2002- 0672.
4. Thomas, R. H., Kinzie K. W. and Pao, S. P., "Computational Analysis of a Pylon-Chevron Core Nozzle Interaction," AIAA 2001-2185.
5. Pope, S. B., "An explanation of the roundjet/ plane-jet anomaly," AIAA Journal, vol. 16, No. 3, 1978.
6. Dash, S. M., Kenzakowski, D. C., Seiner, J.M. and Bhat, T. R. S., "Recent Advances in Jet Flowfield Simulation: Part I - Steady Flows," AIAA-93-4390, October, 1993.
7. Thies, A. T. and Tam, C. K. W., "Computation of Turbulent Axisymmetric and Nonaxisymmetric Jet Flows Using the K-ε Model," AIAA Journal Vol. 34, No. 2, p.309-316, February 1996.
8. Wilcox, D. C., Turbulence Modeling for CFD, Second Edition, DCW Industries, Inc., 1998.
9. Lebedev, A. B., Lyubimov, D A., Maslov, V.P., Mineev, B. I, Secundov, A. N. and Birch S. F. "The Prediction of Three- Dimensional Flows for Noise Applications," AIAA-2002-2422.
10. Pope, S. B, Turbulent Flows, Cambridge University Press, 2000.
11. Birch, S. F., "Turbulence Models - Progress and Problems," Computer Methods in Fluids, Eds., K. Morgan, C. Taylor and C. A. Brebbia, pp. 285-307, Pentech Press,1980.
12. Rubel, A., "On Vortex Stretching Modification of the k-ε Model: Radial Jets," AIAA J. Vol. 23, No. 7, pp. 1129-1130, July 1985.
13. C.K.W. Tam, A. Ganesan., "A modified k-ε Turbulence Model for Calculating the Mean Flow and Noise of Hot Jets," AIAA-2003- 1064, January 2003.
14. Papp, J. L. and Dash, S. M., "Turbulence Model Unification and Assessment for High- Speed Aeropropulsive Flows," AIAA-2001- 0880, January 2001.
15. Schlichting, H, Boundary Layer Theory, Fourth Edition, McGraw Hill Book Co, 1960.
16. Newman, B. G., "Turbulent Jets and Wakes in a Pressure Gradient," Fluid Mechanics of Internal Flow, (Ed. G. Sorvan), Elsevier, p. 170., 1967.
17. Wygnanski, I. and Fiedler, H. "Some Measurements in the Self-Preserving Jet," J. Fluid Mech. vol. 38, part 3, pp. 577-612, 1969.
18. Rodi, W. "The Prediction of Free Turbulent Boundary Layers by Use of a Two-Equation Model of Turbulence," Ph.D. Thesis, Imperial College, London, December 1972.
19. Rodi, W. "A Review of Experimental Data of Uniform Density Free Turbulent Boundary Layers," in Studies in Convection Vol. I, Ed. B. E. Launder, Academic Press, London, 1975.
20. Hussein, J. H., Capp, S. P. and George, W. K. "Velocity Measurements in a High- Reynolds-Number, Momentum- Conserving, Axisymmetric Jet," J. Fluid Mech. vol. 258, pp. 31-75, 1994.
21. Panchapakesan, N. R. and Lumley, J. L. "Turbulence Measurements in Axisymmetric Jets of Air and Helium. Part 1. Air Jet," J. Fluid Mech. vol. 246, pp.197-223. 1993.
22. B.F. Launder, B.L. Sharma. "Application of the Energy-Dissippation Model of Turbulence to the Calculation of Flow Near a Spinning Disc," Letters in Heat and Mass Transfer, 1974, vol. 1, pp. 131-138.
23. Hill, W. G., Jenkins, R. C. and Gilbert, B. L. "Effects of Initial Boundary Layer Conditions on Jet Mixing," Grumman Research Department report RE-509, September 1975.
24. Higgins C. C. and Wainwright, T. W. "Dynamic Pressure and Thrust Characteristics of Cold Jets Discharging from Several Exhaust Nozzles Designed for VTOL Downwash Suppression," NASA TN D-2263, 1964.
25. Lepicovsky, J., Ahuja, K. K., Brown, W. H., Salikuddin, M. and Morris, P. J., "Acoustically Excited Heated Jets, Part III - mean Flow Data," NASA Contractor Report 4129, June 1988.