Parameterization of Boundary-Layer Transition Induced by Isolated Roughness Elements
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of Rome “La Sapienza”, 00184 Rome, Italy
2. Department of Aeronautics and Astronautics, Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052842
Reference28 articles.
1. X-33 Hypersonic Boundary-Layer Transition
2. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
3. Review of Published Data on the Effect of Roughness on Transition from Laminar to Turbulent Flow
4. The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic Speeds
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2. Numerical investigation of a Mach 6 laminar shock-wave/boundary-layer interaction on a two-dimensional ramp with 3D controlled surface roughness;International Journal of Heat and Fluid Flow;2023-10
3. Roughness Parameter Optimization of the McClain Model in GlennICE;SAE Technical Paper Series;2023-06-15
4. Sensitivity of Boundary Layer Transition to Roughness Spacing and Acoustic Forcing;Proceeding of 10th International Symposium on Turbulence, Heat and Mass Transfer, THMT-23, Rome, Italy, 11-15 September 2023;2023
5. Sensitivity of Boundary Layer Transition to Roughness Spacing and Acoustic Forcing;Proceeding of 10th International Symposium on Turbulence, Heat and Mass Transfer, THMT-23, Rome, Italy, 11-15 September 2023;2023
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