Items where Author is "Cerminara, Adriano"
Number of items: 15.
Article
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.
[Article]
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.
[Article]
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.
[Article]
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.
[Article]
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.
[Article]
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.
[Article]
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.
[Article]
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.
[Article]
Book Section
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.
[Book Section]
Conference or Workshop Item
NAYAK, Raahil, CERMINARA, Adriano and POTTS, Jonathan
(2024).
Transpiration Cooling Strategies and their Impact on Hypersonic Boundary Layer Flow [abstract only].
In: UK Fluids 2024, Swansea, UK, 09-11 Sep 2024.
[Conference or Workshop Item]
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.
[Conference or Workshop Item]
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.
[Conference or Workshop Item]
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.
[Conference or Workshop Item]
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.
[Conference or Workshop Item]
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.
[Conference or Workshop Item]