Turbulence Modeling Effects on Calculation of Lobed Nozzle Flowfields
Author:
Affiliation:
1. NASA John H. Glenn Research Center, Lewis Field, Cleveland, Ohio 44135
2. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.17160
Reference24 articles.
1. Assessment of Parameters Influencing the Prediction of Shear-Layer Mixing
2. A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields
3. Turbulence Modeling Improvements for Jet Noise Prediction Using PIV Datasets
4. EASM/J Extensions and Evaluation for Jet Noise Prediction
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