0
TECHNICAL PAPERS

Temperature Corrected Turbulence Model for High Temperature Jet Flow

[+] Author and Article Information
Khaled S. Abdol-Hamid, S. Paul Pao

Configuration Aerodynamics Branch, MS 499, NASA Langley Research Center, Hampton, VA 23681

Steven J. Massey

Eagle Aeronautics, Inc., 13 West Mercury Blvd., Hampton, VA 23669

Alaa Elmiligui

Analytical Services & Materials, Inc., 107 Research Dr., Hampton, VA 23660

J. Fluids Eng 126(5), 844-850 (Dec 07, 2004) (7 pages) doi:10.1115/1.1792266 History: Received July 18, 2003; Revised May 12, 2004; Online December 07, 2004
Copyright © 2004 by ASME
Your Session has timed out. Please sign back in to continue.

References

PAB3D Code Manual Originally developed by the Propulsion Aerodynamics Branch, now under cooperative program between the Configuration Aerodynamics Branch, NASA Langley Research Center and Analytical Services & Materials, Inc. Hampton, VA. See http://www.asm-usa.com/software/pab3d.html.
Seiner, J. M., Ponton, M. K., Jansen, B. J., and Lagen, N. T., 1992, “The Effects of Temperature on Supersonic Jet Noise Emission,” DGLR/AIAA 14th Aeroacoustics Conference, Aachen, Germany, AIAA Paper No. 92-02-046, May 1992.
Thomas, R. H., Kinzie, K. W., and Pao, S. Paul, 2001, “Computational Analysis of a Pylon-Chevron Core Nozzle Interaction,” AIAA Paper 2001-2185, May 2001.
DeBonis, J. R., and Scott, J. N., 2001, “A Large-Eddy Simulation of a Turbulent Compressible Round Jet,” AIAA Paper 2001-2254, May 2001.
Georgiadis, N. J., Alexander, J. I. D., and Reshotko, E., 2001, “Development of a Hybrid RANS/LES Method for Compressible Mixing Layer Simulations,” AIAA Paper 2001-0289, Jan. 2001.
Jones,  W. P., and Launder,  B. E., 1972, “The Prediction of Laminarization With a Two-Equation Model of Turbulence,” Int. J. Heat Mass Transfer, 15, pp. 301–314.
Sarkar,  S., Erlebacher,  G., Hussaini,  M. Y., and Kreiss,  H. O., 1991, “The Analysis and Modeling of Dilatational Terms in Compressible Turbulence,” J. Fluid Mech., 227, pp. 473–495.
Wilcox, David C., 1987, “Progress in Hypersonic Turbulence Modeling,” AIAA 91-1785, June 1991; Vol. 109, June 1987, pp. 156–160.
Theis,  A. T., and Tam,  C. K. W., 1996, “Computation of Turbulent Axisymmetric and Non-Axisymmetric Jet Flows Using the k-ε Model,” AIAA J., 34, pp. 309–316.
Tam, C. K. W., and Ganesan, A., 2003, “A Modified k-ε Model for Calculating the Mean Flow and Noise of Hot Jets,” AIAA 2003-1064, January 2003.
Lebedev, A. B., Lyubimov, A. D., Maslov, V. P., Mineev, B. I., Secundov, A. N., and Birch, Stanley F., 2002, “The Prediction of Three-Dimensional Jet Flows for Noise Applications,” AIAA 2002–2422, 2002.
So,  R. M. C., and Sommer,  T. P., 1995, “An Explicit Algebraic Heat-Flux Model for the Temperature Field,” Int. J. Heat Fluid Flow, 7, pp. 455–465.
Ronki,  M., and Gatski,  Thomas B., 2001, “Predicting Turbulent Convective Heat Transfer in Fully Developed Duct Flows,” Int. J. Heat Fluid Flow, 22, pp. 381–392.
Abe,  K., Kondoh,  T., and Nagano,  Y., 1996, “A Two-Equation Heat Transfer Model Reflecting Second-Moment Closures for Wall and Free Turbulent Flows,” Int. J. Heat Fluid Flow, 17, pp. 228–237.
Dembowski, M. A., and Georgiadis, N. J., 2002, “An Evaluation of Parameters Influencing Jet Mixing Using the WIND Navier-Stokes Code,” NASA TM 2002-211727, 2002.
Massey, S. J., Thomas, R. H., Abdol-Hamid, K. S., and Elmiligui, A., 2003, “Computational and Experimental Flowfield Analyses of Separate Flow Chevron Nozzles and Pylon Interaction,” AIAA-2003-3212.
Hunter, C., Pao, S., and Thomas, R., 2003, “Development of a Jet Noise Prediction Method for Installed Jet Configurations,” AIAA 2003-3169.
Birch, Stanley F., Lyubimov, D. A., Secundov, A. N., and Yakubovsky, K. Ya., 2003, “Numerical Modeling Requirements for Coaxial and Chevron Nozzle Flows,” AIAA Paper 2003-3287.

Figures

Grahic Jump Location
Computational grid for the supersonic jet flow
Grahic Jump Location
A comparison of computed results for coarse, medium and fine grid level and data 16
Grahic Jump Location
Comparison of computed center line stagnation temperature and data 16
Grahic Jump Location
A comparison of the stagnation temperature prediction with data 16
Grahic Jump Location
Computational domain for the mutistream jet flow
Grahic Jump Location
Configuration 1, baseline round core nozzle with round fan nozzle
Grahic Jump Location
Configuration 4, 8-chevron core nozzle with round fan nozzle and pylon
Grahic Jump Location
A comparison of solutions at Tt=2009.67 R using different turbulence models with data 2
Grahic Jump Location
A comparison of solutions at Tt=1359.67 R using different turbulence models with data 2
Grahic Jump Location
A comparison of solutions at Tt=563.67 R using different turbulence models with data 2

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In