

Price Jr., E.A., Stallings Jr., R.L.: Investigation of turbulent separated flows in the vicinity of fin-type protuberances at supersonic Mach numbers. īrusniak, L., Dolling, D.S.: Physics of unsteady blunt-fin-induced shock wave/turbulent boundary-layer interaction. ĭolling, D.S., Bogdonoff, S.M.: Blunt fin-induced shock wave/turbulent boundary-layer interaction. ĭolling, D.S., Bogdonoff, S.M.: Scaling of interactions of cylinders with supersonic turbulent boundary layers. Westkaemper, J.C.: Turbulent boundary-layer separation ahead of cylinders. Hung, F.T., Greenschlag, S.N., Scottoline, C.A.: Shock-wave-boundary-layer interaction effects on aerodynamic heating. īlevins, R.D., Holehouse, I., Wentz, K.R.: Thermoacoustic loads and fatigue of hypersonic vehicle skin panels. Korkegi, R.H.: Survey of viscous interactions associated with high Mach number flight. Holden, H.A., Babinsky, H.: Separated shock-boundary-layer interaction control using streamwise slots. Knight, D.D., Yan, H., Panaras, A.G., Zheltovodov, A.A.: Advances in CFD prediction of shock wave turbulent boundary layer interactions. 203 (1975)ĭélery, J., Marvin, J.: Shock-wave boundary-layer interactions. Hankey Jr., W.L., Holden, M.S.: Two-dimensional shock wave-boundary layer interactions in high speed flows. Knight, D.D., Degrez, G.: Shock wave boundary layer interactions in high Mach number flows: a critical survey of current numerical prediction capabilities.

Ĭlemens, N.T., Narayanaswamy, V.: Low-frequency unsteadiness of shock wave/turbulent boundary layer interactions.

ĭolling, D.S.: Fifty years of shock-wave/boundary-layer interaction research: what next? AIAA J.

Gaitonde, D.V.: Progress in shock wave/boundary layer interactions. While the position and structure of the interaction may change as a result of varying \(d/\delta \), the effects on the unsteady dynamics were minimal. The characteristic interaction variables (the maximum separation distance, S, and the triple-point height, \(h_\mathrm\)) content. This was found to be an appropriate scaling parameter for mean features. The primary interaction variable, the cylinder diameter ( d), and a secondary interaction variable, the boundary-layer thickness ( \(\delta \)), were varied to study the effects of the parameter \(d/\delta \). Scaling parameters of shock-wave/turbulent boundary-layer interactions generated by a semi-infinite standing cylinder were explored in a combined numerical and experimental effort, consisting of Reynolds-averaged Navier–Stokes simulations and high-speed schlieren imaging.
