1. Transonic shock wave—boundary-layer interactions;Babinsky,2014
2. Confinement effects in shock wave/turbulent boundary layer interactions through wall-modelled large-eddy simulations;Bermejo-Moreno;J Fluid Mech,2014
3. Leading edge bluntness effect on the flow in a model air-inlet;Borovoy;Fluid Dyn,2014
4. Bravo-Mosquera PD, Cerón-Muñoz HD, Catalano FM. Analytical and numerical design of a mixed-compression air intake for a supersonic fighter aircraft. In: 1° Simpósio do Programa de Pós-Graduação em Engenharia Mecânica, Universidade de São Paulo, 12 e 13 de setembro de 2016, São Carlos, São Paulo, Brasil. https://ru.scribd.com/document/355910642/Analytical-and-Numerical-Design-of-a-Mixed-compression-Air-Intake-for-a-Supersonic-Fighter-Aircraft (accesses Accessesedon August 20, 2018).
5. Experimental and numerical investigation on hysteresis characteristics and formation mechanism for a variable geometry dual-mode combustor;Feng;Aerosp Sci Technol,2017