Flow field comparisons from three Navier-Stokes solvers for an axisymmetric separate flow jet
Author:
Affiliation:
1. NASA, Glenn Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-672
Reference24 articles.
1. Kenzakowski, D.C., Shipman, J., Dash, S.M., Bridges, J., and Saiyed, N. "Study of Two-stream Laboratory Jets with Passive Mixing Enhancements for Noise Reduction,"AIAA-2000-0219.
2. Georgiadis, N.J., Yoder, D.A., and DeBonis, J.R. "A Comparison of Three Navier-Stokes Solvers for Exhaust Nozzle Flowfields," NASA/TM-1999-209184.
3. Hamed, A., Khavaran, A., and Lee, S. "The Flow and Acoustic Predictions for a High By-Pass Ratio Exhaust Nozzle,"AIAA-98-3257.
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