Reynolds Number Effects on Shock Wave Boundary Layer Interaction in a Hypersonic Flow

Srinath, L., Mohammed Ibrahim, S., Sriram, R., Reddy, K. P. J., & Jagadeesh, G. (2019). Reynolds Number Effects on Shock Wave Boundary Layer Interaction in a Hypersonic Flow. In 31st International Symposium on Shock Waves 1 (pp. 993–999). Springer International Publishing. https://doi.org/10.1007/978-3-319-91020-8_119