Calibration and validation of EASM turbulence model for jet flowfields

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Papp, J ^a   Kenzakowski, D C ^a   Dash, S M ^a  

^a Combustion Research and Row Technology Inc ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; TURBULENCE MODELS;

CALIBRATION AND VALIDATIONS; COMPLEX FLOW; EXPLICIT ALGEBRAIC STRESS MODEL; MIXING LAYERS; MODEL FRAMEWORK; MODEL RESULTS; ROUND JETS; TEST CASE;

FLOW FIELDS;

EID: 85086612914     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-855     Document Type: Conference Paper

References (38)

1. Papp, J. L., and Dash, S. M., "Turbulence Model Unification and Assessment for High-Speed Aeropropulsive Flows", AIAA-2001-0880, 2001.
2. Calhoon, W. H., and Kenzakowski, D. C., "Flowfield and Radiation Analysis of Missile Exhaust Plumes Using a Turbulent-Chemistry Interaction Model", AIAA-2000-3388.
3. Kenzakowski, D.C., Shipman, J.D., and Dash, S.M., and P. Markarian, M. Borger and G. Smith, Lockheed Martin, "High-Fidelity Simulations Of Aircraft Plume Signatures, " The 2001 Electromagnetic Code Consortium (EMCC) Annual Meeting and the Multidisciplinary University Research Initiative (MURI) review to be held at the Sheraton Kauai Hotel, in Kauai, Hawaii, on 28 May-1 June,2001.
4. Herrin, J. L., and Dutton, J. C., "Supersonic Base Flow Experiments in the Near Wake of a Cylindrical Afterbody", AIAA Journal Vol. 32, No. 1, pp. 77-83, 1994.
5. Gruber, M., Messersmith, N. L., and Dutton, J. C., "Three-Dimensional Velocity Field in a Compressible Mixing Layer", AIAA Journal, Vol. 31, No. 11, pp. 2061-2067, 1993.
6. Khavaran, Abbas, "Role of Anisotropy in Turbulent Mixing Noise", AIAA Journal, Vol. 37, No. 7, pp. 832-841, 1999.
7. Gatski, T. B., and Speziale, C. G., "On explicit algebraic stress models for complex turbulent flows", J. of Fluid Mech., Vol. 254, pp. 59-78, 1993.
8. Abid, R., Morrison, J. H., Gatski, T. B., and Speziale, C. G., "Prediction of Complex Aerodynamic Flows with Explicit Algebraic Stress Model", AIAA 96-0565.
9. Kenzakowski, D. C., Papp, J. L., and Dash S. M., "Evaluation of Advanced Turbulence Models and Variable Prandtl/Schmidt Number Methodology for Propulsive Flows", AIAA 2000-0885, 2000.
10. Gatski, T. B., and Jongen, T., "Nonlinear eddy viscosity and algebraic stress models for solving complex turbulent flows, " Progress in Aerospace Sciences, 36, pp. 655-682, 2000.
11. Jongen, T., and Gatski, T. B., "A New Approach to Characterizing the Equilibrium States of Reynolds Stress Anistropy in Homogeneous Turbulence, " Theoret. Comput. Fluid Dynamics, 11, pp. 31-47, 1998.
12. Rumsey, C. L. and Gatski, T. B., "Isolating Curvature Effects In Computing Wall-Bounded Turbulent Flows", AIAA-2001-0725, 2001.
13. Kenzakowski, D.C., Papp, J.L., and Dash, S.M., "Modeling Turbulence Anisotropy For Jet Noise Prediction, " AIAA 2002-0076, 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 14-17, 2002.
14. Speziale, C. G., Sarkar, S. Gatski, T. B., "Modelling the pressure-strain correlation of turbulence: an invariant dynamical systems approach, " J. of Fluid Mech., vol. 227, pp. 245-272, 1991.
15. Girimaji, S. S., "Fully-Explicit and Self-Consistent Algebraic Reynolds Stress Model, " ICASE Report No. 95-82, 1995.
16. Pope, S., "An Explanation of the Turbulent Round-Jet/Plane-Jet Anomaly", AIAA Journal, Vol. 16, No. 3, 1978, pp. 279-281.
17. Launder, B. E., and Sharma, B. I., "Application of the Energy Dissipation Model of Trubulence to the Calculation of Flow Near a Splinning Disc, " Leeters in Heat and Mass Transfer, Vol. 1, No. 2, pp. 131-138, 1974.
18. Compte-Bellot, G. and Corrsin, S., "Simple Eularian time Correlation of Full-and Narro-Band Velocity signals in Grid Generated Isotrpic Turbulence, " J. of Fluid Mech., Vol. 48, pp. 273-337, 1971.
19. Tavoularis, S. and Karnik, U., "Further Experiments on the Evolution of Turbulent Stresses and Scales in Uniformly Sheard turbulence, " J. of Fluid Mech., Vol. 224, p. 457, 1989.
20. Tavoularis, S., and Corrsin, S., "Experiments in Nearly Homogeneous Turbulent Shear Flow with Uniform Mean Temperature Gradient, Part I, " J. of Fluid Mech., Vol., 104, pp. 311-347, 1981.
21. Lee, M. J., and Reynolds, W. C., "Numerical experiments on the structure of homogenous turbulence" Stanford Univ. Tech. Rep. TF-24, 1985.
22. York, B.J., Kenzakowski, D.C., Lee, R.A., and Dash, S.M., "Upgrades to CRAFT Code for Simulation of Ducted Launcher/Plume Interactions, " 1997. JANNAF EPTS & SPIRITS Users Group Joint Meeting, Lockheed Martin Corp., Sunnyvale, CA, 7-11 April 1997.
23. Patel, R. P., "An Experimental Study of a Plane Mixing Layer, " AIAA Journal, Vol. 11, No. 1, pp. 67-71, 1973.
24. Bradbury, L. J. S., "The Structure of a Self-Preserving Turbulent Plane Jet, " J. of Fluid Mech., Vol. 23, Pt. 1, pp. 31-64, 1965.
25. Weinstein, A. S., Osterle, J. F., and Forstall, W., "Momentum Diffusion from a Slot Jet into Moving Secondary, " J. of Applied Mech., pp. 437-443, 1956.
26. Antonia, R. A., and Bilger, R. W., "An Experimental Investigation of an Axi-symmetric Jet in a Co-Flowing Air Stream, " J. of Fluid Mech., Vol. 61, Pt. 4, pp. 805-822, 1973.
27. Rodi, W., "The Prediction of Free turbulent Boundary layers by the Use of a Two-Equation Model of Turbulence, " Ph.D. Thesis, Univ. of London, 1972.
28. Wygnanski, L. and Fiedler, H. "Measurements in the Self-Preserving Jet, " J. of Fluid Mech., Vol. 38, Pt. 3, pp. 577-612, 1969.
29. Dash, S.M., "Observations on Practical Turbulence Modeling for High-Speed Jet/Plume Flowfields, " AIAA 22nd Fluid and Plasmadynamics Conference, AIAA-91-1789, Honolulu, Hawaii, June 24-26, 1991.
30. Dash, S.M., Walker, B.J., and Seiner, J.M., "A Building-Block Approach for Turbulence Model Validation/Upgrade Focused on High-Speed Flows, " 19th JANNAF Propulsion Meeting, Feb. 24-27, 1992.
31. Hussein, J. H., Capp, S. P., and George, W. K., "Velocity measurements in a high-Reynolds number momentum-conserving, axisymmetric, turbulent jet, " J. of Fluid Mech., Vol. 258, pp. 31-75, 1994.
32. Eggers, J. M., "Velocity Profiles and Eddy Viscosity Distributions Downstream of a Mach 2.22 Nozzle Exhausting to Quiescent Air, " NASA TN D-3601, 1966.
33. Seiner, J.M., Ponton, M.K., Jansen, B.J. and Lagen, N.T., "The Effects of Temperature on Supersonic Jet Noise Emission, " DGRL/AIAA 92-02-046, DGLR/AIAA 14th Aeroacoustics Conference, Aachen, Germany, May 11-14, 1992.
34. Kenzakowski, D.C., Papp, J., and Dash, S.M., "Evaluation of Advanced Turbulence Models and Variable Prandtl/Schmidt Number Methodology for Propulsive Flows, " AIAA Paper No. 2000-0885, 38th AIAA Aerospace Sciences Meeting at Reno, NV, Jan. 10-13,2000.
35. Seiner, J.M., Ukeiley, L.S., Ponton, M.K., and Papp, J.L., "Jet Turbulence Measurements of Aeroacoustic Source Using Stereo PIV, " AIAA-2001-2184, 7th AIAA/CEAS Aeroacoustics Conference, The Maastricht Exhibition and Congress Centre, Maastricht, The Netherlands, May 28-30, 2001.
36. Bridges, J., "Measurements of Turbulent Flow Field in Separate Flow Nozzles with Enhanced Mixing Devices-Test Report, " Paper No. AIAA-2000-1961, 6th AIAA/CEAS Aeroacoustics Conference, Lahaina, Hawaii, June 12-14, 2000.
37. Sturek, W. B., Birch, T., Lauzon, M., Housh, C., Manter, J., Josyula, E., Soni, B., "The Application of CFD to the Prediction of Missile Body Vortices, " AIAA Paper No. 97-0637, 35th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan., 6-10, 1997.
38. Hosangadi, A., Lee, R. A., Cavallo, P. A., Sinha, N., "Hybrid, Viscous, Unstructured Mesh Solver for Propulsive Applications, " AIAA Paper No. 98-3153, 34th Joint Propulsion Conference & Exhibit, Cleveland, OH, July 13-15, 1998.