This dataset was generated to analyze the effects of a nonadiabatic wall on hypersonic shock/boundary-layer interactions and is related to the following publication: Volpiani, P. S., Bernardini, M., & Larsson, J. (2020). Effects of a nonadiabatic wall on hypersonic shock/boundary-layer interactions. Physical Review Fluids, 5(1), 014602. The database contains instantaneous and statistical fields of hypersonic boundary layers and shock/boundary-layer interactions at free-stream Mach number 5. We considered different wall thermal conditions and a wide range of deflection angles. Python scripts are also provided to analyze the data.

P.S.V. and J.L. were supported by the Air Force Office of Scientific Research (Grant No. FA9550-16-1-0385). M.B. was supported by the Scientific Independence of young Researchers program 2014 (Active Control of Shock-wave Boundary-layer Interaction project, Grant No. RBSI14TKWU), funded by MIUR. The work was performed using HPC resources of the University of Maryland (DeepThought2), the Maryland Advanced Research Computing Center (MARCC), and the Argonne Leadership Computing Facility, which is a DOE Office of Science User Facility supported under Contract No. DE-AC02-06CH11357.

{"references": ["Volpiani, P. S., Bernardini, M., & Larsson, J. (2020). Effects of a nonadiabatic wall on hypersonic shock/boundary-layer interactions. Physical Review Fluids, 5(1), 014602."]}