Uncertainty Analysis of Inflow Parameters for Mid-Lift-to-Drag Vehicle Transition
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060387
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3. HollisB. R.HollingsworthK. E. “Experimental Aeroheating Study of Mid-L/D Entry Vehicle Geometries: NASA LaRC 20-Inch Mach 6 Air Tunnel Test 6966,” NASA TM-2014-218549, 2014.
4. A Three-Equation Eddy-Viscosity Model for Reynolds-Averaged Navier–Stokes Simulations of Transitional Flow
5. Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes
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