Items where Author is "Cerminara, Adriano"

SHARMA, Pushpender, DEITERDING, Ralph, CERMINARA, Adriano and SANDHAM, Neil (2023). Numerical simulation of transpiration cooling for a high-speed boundary layer undergoing transition to turbulence. Aerospace Science and Technology, 141: 108581.

CERMINARA, Adriano (2023). Turbulence Effect on Transpiration Cooling Effectiveness Over a Flat Plate in Hypersonic Flow and Sensitivity to Injection Parameters. Flow, Turbulence and Combustion, 110 (4), 945-968.

CERMINARA, Adriano, HERMANN, Tobias, IFTI, Hassan Saad, DEITERDING, Ralf, SANDHAM, Neil and MCGILVRAY, Matthew (2021). Influence of instability modes on cooling performance in hypersonic boundary layer with slot injection. Aerospace Science and Technology, 109: 106409.

CERMINARA, Adriano, DEITERDING, Ralf and SANDHAM, Neil (2020). A mesoscopic modelling approach for direct numerical simulations of transition to turbulence in hypersonic flow with transpiration cooling. International Journal of Heat and Fluid Flow, 86: 108732.

CERMINARA, Adriano and SANDHAM, Neil (2020). Transition mechanisms in cross-flow-dominated hypersonic flows with free-stream acoustic noise. Journal of Fluid Mechanics, 896: A21.

CERMINARA, Adriano, DURANT, Antoine, ANDRÉ, Thierry, SANDHAM, Neil D and TAYLOR, Nigel J (2018). Receptivity to Freestream Acoustic Noise in Hypersonic Flow over a Generic Forebody. Journal of Spacecraft and Rockets, 56 (2), 447-457.

WAGNER, Alexander, SCHÜLEIN, Erich, PETERVARI, René, HANNEMANN, Klaus, ALI, Syed RC, CERMINARA, Adriano and SANDHAM, Neil D (2018). Combined free-stream disturbance measurements and receptivity studies in hypersonic wind tunnels by means of a slender wedge probe and direct numerical simulation. Journal of Fluid Mechanics, 842, 495-531.

CERMINARA, Adriano and SANDHAM, Neil D (2017). Acoustic Leading-Edge Receptivity for Supersonic/Hypersonic Flows over a Blunt Wedge. AIAA Journal, 55 (12), 4234-4244.

CERMINARA, Adriano, LEVIN, Deborah A and THEOFILIS, Vassilios (2023). Shock receptivity: characteristics of shock oscillation modes and induced boundary-layer disturbances. In: AIAA SCITECH 2023 Forum. Reston, VA, American Institute of Aeronautics and Astronautics.

CERMINARA, Adriano, LEVIN, Deborah A. and THEOFILIS, Vassilis (2024). Susceptibility of shock-transitional-boundary-layer interaction to shock oscillations in hypersonic flow. In: AIAA SCITECH 2024 Forum, Orlando, FL, USA, 08-12 Jan 2024. American Institute of Aeronautics and Astronautics.

CERMINARA, Adriano, DURANT, Antoine, ANDRÉ, Thierry, SANDHAM, Neil and TAYLOR, Nigel J. (2018). DNS of acoustic receptivity and breakdown in a Mach 6 flow over a generic forebody. In: 2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida, 08–12 January 2018. American Institute of Aeronautics and Astronautics.

CERMINARA, Adriano and SANDHAM, Neil (2016). Boundary-layer receptivity and breakdown in hypersonic flow over a swept blunt wedge with three-dimensional freestream acoustic disturbances. In: 8th AIAA Flow Control Conference, Washington, D.C., 13-17 June 2016. American Institute of Aeronautics and Astronautics.

KONTOGIANNIS, Konstantinos, CERMINARA, Adriano, TAYLOR, Nigel J., SOBESTER, Andras and SANDHAM, Neil (2015). Parametric geometry models for hypersonic aircraft components: blunt leading edges. In: 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. American Institute of Aeronautics and Astronautics.

CERMINARA, Adriano and SANDHAM, Neil (2015). Leading-edge receptivity to acoustic waves for high-speed flows over a blunt wedge. In: 45th AIAA Fluid Dynamics Conference, Dallas, TX, 22-26 Jun 2015. American Institute of Aeronautics and Astronautics.