PAB3D: Its history in the use of turbulence models in the simulation of jet and nozzle flows

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 8, Issue , 2006, Pages 5871-5895

  Abdol Hamid, Khaled S ^a,d   Pao, S Paul ^a,d   Hunter, Craig A ^a,d   Deere, Karen A ^a,d   Massey, Steven J ^b,d   Elmiligui, Alaa ^c,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Eagle Aeronautics Inc   (United States)

^c ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

SUPERSONIC JETS; TEMPERATURE MIXING; TRANSITION FUNCTIONS;

COMPUTATIONAL METHODS; COMPUTER SIMULATION; NAVIER STOKES EQUATIONS; NOZZLES; NUMERICAL METHODS; SUPERSONIC AIRCRAFT; TURBULENCE MODELS;

JET AIRCRAFT;

EID: 34347247291     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (66)

1. Reichardt, Hans: Gesetzmässigkeiten der freien Turbulenz. VDI-Forschungsh. 414, 1942.
2. Görtier, H. "Berechnung von Aufgaben der freien Turbulenz auf Grund eines neuen Näherungsansatzes. Z. Angew. Math. Mech, " Bd. 22, Nr. 5, Oct. 1942, pp. 244-254.
3. Warren, Walter R., Jr. "An Analytical and Experimental Study of Compressible Free Jets." Publ. No.: 23, 885, Univ. Microfilms, Inc., 1957.
4. Abramovich, G. N.: The Theory of Turbulent Jets. M.I.T. Press, 1963.
5. Love, Eugene S. Grigsby, Carl E., Lee, Louise P., and Woodling, Mildred J. "Experimental and Theoretical Studies of Axi symmetric Free Jets" NASA TR R-6, 1959. (Supersedes NACA RM L54L31 by Love and Grigsby, RM L55J14 by Love, RM L56G18 by Love, Woodling, and Lee, and TN 4195 by Love and Lee.)
6. Dash, Sanford M., and Wolf, David E. "Fully-Coupled Analysis of Jet Mixing Problems, Part I," ShockCapturing Model, SCIPVIS. NASA CR-3716, 1984.
7. Dash, Sanford M., Pergament, Harold S., and Thorpe, Roger D. "Computational Models for the Viscousllnviscid Analysis of Jet Aircraft Exhaust Plumes" NASA CR-3289, 1980.
8. Seiner, John M. "Advances in High Speed Jet Aeroacoustics," AIAA-84-2275, Oct. 1984.
9. Seiner, J. M., and Norum, T. D. "Aerodynamic Aspects of Shock Containing Jet Plumes," AIAA-80-0965, June 1980.
10. Abdol-Hamid, Khaled S., and Wilmoth, Richard G. "Multiscale Turbulence Effects in Underexpanded Supersonic Jets," AIAA J., vol. 27, Mar. 1989, pp. 315-322.
11. Abdol-Hamid, Khaled S. "The Application of 3D Marching Scheme for the Prediction of Supersonic Free Jets," AIAA/ASME/AE/ and ASEE 25th Joint Propulsion Conference, July 1989. (Available as AIAA-892897.)
12. Abdol-Hamid, Khaled S., Uenishi, Kenji, and Turner, William "Three-Dimensional Upwinding Navier-Stokes Code With k-ε Model for Supersonic Flows," AIAA-91-1669, June 1991.
13. Seiner, J.M., Ponton, M.K., Jansen, B. J., and Lagen, N. T., "The Effects of Temperature on Supersonic Jet Noise Emission," DGLR/AIAA 14th Aeroacoustics Conference, Aachen, Germany, AIAA Paper No. 92-02046, May 1992.
14. Thomas, R.H., Kinzie, K.W. and Pao, S. Paul, "Computational Analysis of a Pylon-Chevron Core Nozzle Interaction," AIAA Paper 2001-2185, May 2001.
15. Theis, A. T., and Tarn, C. K. W., "Computation of Turbulent Axisymmetric and Non-axisymmetric Jet Flows Using the k-e Model," AIAA Journal, Vol. 34, No. 2, February 1996, pp. 309-316.
16. Tam, C. K.W., and Ganesan, A., "A Modified k-ε Model for Calculating the Mean Flow and Noise of Hot Jets," AIAA 2003-1064, January 2003.
17. Lebedev A. B., Lyubimov A. D., Maslov, V. P., Mineev, B. I., Secundov, A. N., and Birch, Stanley F., "The Prediction of Three-Dimensional Jet Flows for Noise Applications," AIAA 2002-2422, 2002.
18. So, R.M.C., and Sommer, T. P., "An Explicit Algebraic Heat-Flux Model for the Temperature Field," International Journal of Heat and Flow, 1995, Vol. 7, pp. 455-465.
19. Ronki, M., and Gatski, Thomas B., "Predicting Turbulent Convective Heat Transfer in Fully Developed Duct Flows," International Journal of Heat and Flow, Vol. 22, 2001, pp. 381-392.
20. Abe, K., Kondoh, T., and Nagano, Y., "A Two-equation Heat Transfer Model Reflecting Second-Moment Closures for Wall and Free Turbulent Flows," International Journal of Heat and Flow, Vol. 17, 1996, pp. 228237.
21. Abdol-Hamid, K. S., Pao, S, Massey, S. J., and Elmiligui, A., "Temperature Corrected Turbulence Model for High Temperature Jet Flow." ASME Journal of Fluids Engineering, Vol. 126, No 5, September 2004.
22. Jones, W. P., and Launder, B. E. "The Prediction of Laminarization With a Two-Equation Model of Turbulence,"Int. J. Heat & Mass Transf., vol. 15, no. 2, Feb. 1972, pp. 301-314.
23. Spalart, P. R., "Young Person's Guide to Detached Eddy Simulation Grids," NASA CR-2001, 211032, 2001.
24. Nichols, R.H. & Nelson, C.C., "Application of Hybrid RANS/LES Turbulence Models" AIAA 2003-0083, 2003.
25. Mani, M., Paynter, C.C., "Hybrid Turbulence Models for Unsteady Simulation of Jet Flows." AIAA 2002-2959, 2002.
26. Batten, P., Goldberg, U., and Chakravarthy, S., "LNS - An Approach Towards Embedded LES," AIAA Paper 2002-0427, 2002.
27. Girimaji S., Sreenivasan, R., Jeong E., "PANS Turbulence Model For Seamless Transition Between RANS, LES: Fixed-Point Analysis and Preliminary Results." FEDSM2003-45336, Proceedings of ASME FEDSM'03 2003 4th ASME-JSME Joint Fluids Engineering Conferences, July 13-16, Honolulu, Hawaii USA, 2003.
28. Abdol-Hamid, K., and Girimaji, S. "A Two-Stage Procedure Toward the Efficient Implementation of PANS and Other Hybrid Turbulence Models," NASA TM-213260, 2004.
29. Abdol-Hamid, K.,S. "Development of Three-Dimensional Code for the Analysis of Jet Mixing Problem," NASA CR 4200, December 1988.
30. Abdol-Hamid, K.S.: A Multiblock/Multizone code (PAB3D-v2) for the Three-Dimensional Navier-Stokes Equations: Preliminary Applications, NASA CR-182032, 1990.
31. Uenishi, K. and Abdol-Hamid, K.: A Three-Dimensional Upwinding Navier-Stokes Code with k-ε Model for Supersonic Flows", AIAA 22nd Fluid and Plasmadynamic Conference, AIAA 91-1669, June 1991.
32. Abdol-Hamid, K. S.; Lakshmanan, B.; and Carlson, J. R.: Application of Navier-Stokes Code PAB3D with k-ε Turbulence Model to Attached and Separated Flows. NASA TP-3480, January 1995
33. Abdol-Hamid, K. S.: Implementation of Algebraic Stress Models in a General 3-D Navier-Stokes Method (PAB3D). NASA CR-4702, December 1995.
34. Carlson, J. R., "Applications of Algebraic Reynolds Stress Turbulence Models," Journal of Propulsion and Power, Volume 13, Number 5, 1997.
35. Shih, T.H., Zhu, J., and Lumley, J.L., "A New Reynolds Stress Algebraic Equation Model." NASA TM106644, August 1994.
36. Girimaji, S.S., "Fully-Explicit and Self-Consistent Algebraic Reynolds Stress Model," ICASE 95-82, December 1995.
37. Nichols, R.H. & Nelson, C.C., "Application of Hybrid RANS/LES Turbulence Models" AIAA 2003-0083, 2003.
38. Abdol-Hamid, K.S. "Three-Dimensional Calculations for Underexpanded and Over expanded Supersonic Jet Flows," AIAA Paper 89-2196, September 1989.
39. Lakshmanan, B. and Abdol-Hamid, K. S. "Application of Space Marching Procedure for Transport Equation of Turbulence Models." Computational Fluid Dynamics Journal, Vol. 1. No. 3, October 1992.
40. Lakshmanan, B., and Abdol-Hamid, K. S. "Investigation of Supersonic Jet Plumes Using an Improved TwoEquation Turbulence Model." Journal of Propulsion and Power, Volume 10, Number 5, September-October 1994, pp. 736-741.
41. Pao, S. P., and Abdol-Hamid, K. S. "Grid Adaptation to Multiple Functions for Applied Aerodynamic Analysis," Proceedings of the Third International Conference on Numerical Grid Generation, Barcelona, Spain, June 1991.
42. Abdol-Hamid, K. S., Uenishi, K., Keith, B. D., and Carlson, John R. "Commercial Turbofan Engine Exhaust Nozzle Flow Analyses," Journal of Propulsion and Power, Vol. 9, No. 3, May-June 1993.
43. Jones, W.T. and Abdol-Hamid K.S. "Computational Analysis of Drag Reduction Techniques for Afterbody/Nozzle/Empennage Configurations. Aerospace Technology Conference and Exposition," Long Beach, California September 1992.
44. Carlson, J. R., Pao, S. P., Abdol-Hamid, K. S., and Jones, W. T. "Aerodynamic Performance Predictions of Single and Twin Jet Afterbodies," AIAA 95-2622, 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Diego, CA, July 10-12, 1995.
45. Carlson, John R., Abdol-Hamid, K.S., and Pao, S. Paul "Computational Analysis of Vented Supersonic Exhaust Nozzle Using a Multiblock/Multizone Strategy"1 Journal of Propulsion and Power, Vol. 9, No. 6, November-December 1993.
46. Pao, S. P., Carlson, J. R., and Abdol-Hamid, K. S. "Computational Investigation of Circular-to-Rectangular Transition Ducts," Journal of Propulsion and Power, Volume 10, Number 1, January-February 1994, pp. 95100.
47. Carlson, J. R., and Asbury, S. C. "Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds," NASA TP-3440, July 1994.
48. Kuhne, C. M., Uenishi, K., Leon, R. M., Abdol-Hamid, K. S. "CFD Based 3D Aero Analysis System for High-speed Mixer-Ejector Exhaust Nozzles," AIAA 94-2941, 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN, June 27-29, 1994.
49. Walter M. Presz, Jr., Gary Reynolds and Craig Hunter "Thrust Augmentation With Mixer/Ejector Systems," 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, AIAA 2002-0230, January 14-17, 2002.
50. Carlson, John R., and Abdol-Hamid, Khaled S. "Prediction of Static Performance for Single Expansion Ramp Nozzles," AIAA Paper No. 93-2571, AIAA/SAE/ ASME/ASEE 29th Joint Propulsion Conference, June 28-30, 1993.
51. Deere, K. A., and Asbury, S. C. "An Experimental and Computational Investigation of a Translating Throat Single Expansion-Ramp Nozzle." AIAA 96-2540, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Lake Buena Vista, FL, July 1-3, 1996.
52. Deere, K. A. and Asbury, S. C. "Experimental and Computational Investigation of a Translating-Throat, Single-Expansion-Ramp Nozzle," NASA TP-1999-209138, May 1999.
53. Deere, K. A. "PAB3D Simulations of a Nozzle With Fluidic Injection for Yaw Thrust-Vector Control," 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, Ohio, AIAA 98-3254, July 1315, 1998, pp. 12.
54. Hunter, Craig A. and Deere, Karen A. "Computational Investigation of Fluidic Counterflow Thrust Vectoring," AIAA 99-2669, presented at the 35th Annual AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, June 20-23, 1999.
55. st AIAA Applied Aerodynamics Conference, Orlando, FL. AIAA 2003-3800, June 23-26, 2003
56. st AIAA Applied Aerodynamics Conference, Orlando, FL. AIAA 2003-3800, June 23-26, 2003.
57. st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ. AIAA 2005-3502, July 11-13, 2005.
58. Thomas, R. H., Kinzie, K. W., and Pao, S. P. "Computational Analysis of a Paylon-Cheveron Core Nozzle Interaction," 7th A1AA/CEAS Aeroacoustics Conference, Maastricht, The Netherlands, AIAA 2001-2185, May 28-30, 2001
59. Hunter, C., Pao, S. and Thomas, R. "Development of a Jet Noise Prediction Method for Installed Jet Configurations," 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 12-14, 2003, Hilton Head,South Carolina. A1AA 2003-3169.
60. Massey, S.J., Thomas, R.H., Abdol-Hamid, K. S., and Elmiligui, A. "Computational and Experimental Flowfield Analyses of Separate Flow Chevron Nozzles and Pylon Interaction," 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 12-14, 2003, Hilton Head, South Carolina. AIAA-2003-3212.
61. Abdol-Hamid, K.S., Pao, S, Massey, S.J., and Elmiligui, A., "Temperature Corrected Turbulence Model for High Temperature Jet Flow." ASME Journal of Fluids Engineering, Vol. 126, No 5, September 2004.
62. Pao, S. Paul and Abdol-Hamid, K. S. "Numerical Simulation of Jet Aerodynamics Using Three-dimensional Navier-Stokes Method (PAB3D)," NASA TP-3596, September 1996.
63. Abdol-Hamid, K., and Elmiligui, A., "Numerical Study of High Temperature Jet Flow Using RANS/LES and PANS Formulation," AIAA Paper 2005-5092, Toronto, 2005.
64. Elmiligui, A., Abdol-Hamid, K., and Hunter, C. "Numerical Investigation Flow in an Over-Expanded Nozzle with Porous Surfaces", AIAA Paper 2005-4159, Tucson, Arizona, 2005.
65. Eggers, James M.: Velocity Profiles and Eddy Viscosity Distributions Downstream of a Mach 2.22 Nozzle Exhausting to Quiescent Air. NASA TN D-3601, 1966.
66. Bridges, J. and Brown, C., "Parametic Testing on Single Flow Hot Jet," AIAA 2004-2824, 2004.