Evaluation of baldwin-barth turbulence model with an axisymmetric afterbody-exhaust jet flowfield

AIAA Journal

Volumn 31, Issue 9, 1993, Pages 1723-1725

  Kandula, M ^a   Buning, P G ^b  

^a LOCKHEED MARTIN   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS; MATHEMATICAL MODELS; TURBULENT FLOW;

BALDWIN BARTH TURBULENCE MODEL; EXHAUST JET; MIXING LAYER PREDICTION; SEPARATED FLOWS;

JETS;

EID: 0027662804     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.49099     Document Type: Article

References (9)

1. Reubush, D.E., and Runckel, J., “Effect of Fineness Ratio on Boattail Drag on Circular-Arc Boattail Afterbodies Having Closure Ratios of 0.50 with Jet Exhaust Mach Numbers Up to 1.3,” NASATND-7192, May 1973.
2. Mason, N. L., and Putnam, L. E., “Pitot Pressure Measurements in Flow Fields Behind Circular-Arc Nozzles with Exhaust Jets at Subsonic Freestream Mach Numbers,” NASA TM 80169, 1979.
3. Deiwert, G. S., Andrews, A. E., and Nakahashi, K., “Theoretical Analysis of Aircraft Afterbody Flows,”Journal of Spacecraft and Rockets, Vol. 24, No. 6,1987, pp. 496-503.
4. Baldwin, B. S., and Lomax, H., “Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows,” AIAA Paper 78-257, Jan. 1978.
5. Peace, A. J., “Turbulent Flow Predictions for Afterbody Nozzle Geometries Including Base Effects,”Journal of Propulsion and Power, Vol. 7, No. 3,1991, pp. 396-403.
6. Chien, K. Y., “Predictions of Channel and Boundary Layer Flows with a Low-Reynolds-Number Turbulence Model,” AIAA Journal, Vol. 20, No. 1, 1982, pp. 33-38.
7. Baldwin, B. S., and Barth, T. J., “A One-Equation Turbulence Transport Model for High Reynolds Number Wall-Bounded Flows,” NASA TM 102847, Aug. 1990.
8. Kandula, M., and Buning, P. G., “Evaluation of Baldwin-Barth Turbulence Model with Thin-Layer Navier-Stokes Computation of an Axisym-metric Afterbody-Exhaust Jet Flowfield,” AIAA Paper 93-0418, Jan. 1993.
9. Buning, P. G., Chen, W.M., Renze, K.J., Sondak, D., and Chiu, I.T., “OVERFLOW / F3D User’s Manual, Version 1.6n,” NASA Ames Research Center, Moffett Field, CA, Oct. 1991.