Effect of Turbulence Model Uncertainty on Scramjet Isolator Flowfield Analysis
Author:
Affiliation:
1. Missouri University of Science and Technology, Rolla, Missouri 65401
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
Reference34 articles.
1. Isolator-Combustor Interactions in a Direct-Connect Ramjet-Scramjet Experiment
2. BaurleR. A.MiddletonT. F.WilsonL. G. “Reynolds-Averaged Turbulence Model Assessment for a Highly Back-Pressured Isolator Flowfield,” NASA Langley Research Center TR NF1676L-15654, Hampton, VA, Dec. 2012.
3. BaurleR. A.AxdahlE. L. “Uncertainty Quantification of CFD Data Generated for a Model Scramjet Isolator Flowfield,” NASA Langley Research Center TR NF1676L-27196, Hampton, VA, Dec. 2017.
4. Uncertainty Quantification of Turbulence Model Closure Coefficients for Transonic Wall-Bounded Flows
5. Investigation of Turbulence Model Uncertainty for Supersonic/Hypersonic Shock Wave-Boundary Layer Interaction Predictions
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