Numerical and experimental investigation into hypersonic boundary layer transition induced by roughness elements
10.1016/j.cja.2018.12.004
Saved in:
Main Authors: | DONG, H., LIU, S., GENG, X., YANG, L., CHENG, K. |
---|---|
Other Authors: | MECHANICAL ENGINEERING |
Format: | Article |
Published: |
Chinese Journal of Aeronautics
2021
|
Subjects: | |
Online Access: | https://scholarbank.nus.edu.sg/handle/10635/212476 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | National University of Singapore |
Similar Items
-
Direct Numerical Simulation of Self-Similar Turbulent Boundary Layers in Adverse Pressure Gradients
by: Skote, Martin, et al.
Published: (2016) -
Computational simulation of unsteady boundary layer over compliant surfaces
by: WANG ZHENGYI
Published: (2010) -
Application of oil-film interferometry image post-processing technology based on MATLAB
by: Dong, H., et al.
Published: (2021) -
DNS of a single low-speed streak subject to spanwise wall oscillations
by: Negi, Prabal Singh, et al.
Published: (2016) -
HYPERSONIC EIGENVIBRATIONS OF HOMOGENEOUS AND HETEROGENEOUS NANOPARTICLES
by: SUN JINGYA
Published: (2012)