Search Results - "Lugrin, Mathieu"

Ground Tests on BOLT at Mach 7: Cross-Facility Comparison and Stability Analysis.

Authors: Sombaert, Loïc Lugrin, Mathieu Bur, Reynald et al.

Source: AIAA Journal. Jun2025, Vol. 63 Issue 6, p2135-2150. 16p.

Separation and Transition on a Cone-Cylinder-Flare: Computational Investigations.

Authors: Caillaud, Clément Scholten, Anton Kuehl, Joseph et al.

Source: AIAA Journal; Jul2025, Vol. 63 Issue 7, p2615-2634, 19p

Separation and Transition on a Cone-Cylinder-Flare: Experimental Campaigns.

Authors: Benitez, Elizabeth K. Caillaud, Clément McDaniel, Zachary A. et al.

Source: AIAA Journal; Jun2025, Vol. 63 Issue 6, p2162-2181, 20p

Multi-scale study of the transitional shock-wave boundary layer interaction in hypersonic flow.

Authors: Lugrin, Mathieu Beneddine, Samir Garnier, Eric et al.

Source: Theoretical & Computational Fluid Dynamics; Apr2022, Vol. 36 Issue 2, p277-302, 26p

Scaling and Transition Effects on Hollow-Cylinder/Flare Shock/Boundary-Layer Interactions in Wind Tunnel Environments.

Authors: Threadgill, James Hader, Christoph Singh, Ashish et al.

Source: AIAA Journal; Apr2025, Vol. 63 Issue 4, p1228-1242, 15p

Transition mechanisms in hypersonic wind-tunnel nozzles: a methodological approach using global linear stability analysis.

Authors: Lemarquand, Hugo Lugrin, Mathieu Content, Cédric et al.

Source: Flow: Applications of Fluid Mechanics; 2025, Vol. 5, p1-21, 21p

Towards an automated toolset for mesh adapted Navier-Stokes simulation of hypersonic vehicles.

Authors: Lugrin, Mathieu Isnard, Baptiste Benazet, Clément et al.

Source: Comptes Rendus Mécanique. 2025, Vol. 353, p1451-1475. 25p.

Transitional shockwave/boundary layer interaction experiments in the R2Ch blowdown wind tunnel.

Authors: Lugrin, Mathieu Nicolas, François Severac, Nicolas et al.

Source: Experiments in Fluids. Feb2022, Vol. 63 Issue 2, p1-19. 19p.

Subjects: Wind tunnels, Proper orthogonal decomposition, Shock waves, Mach number, Reynolds number

Transition scenario in hypersonic axisymmetrical compression ramp flow.

Authors: Lugrin, Mathieu Beneddine, Samir Leclercq, Colin et al.

Source: Journal of Fluid Mechanics. 1/25/2021, Vol. 907, p1-40. 40p.

Subjects: Mach number, Boundary layer (Aerodynamics), Proper orthogonal decomposition, Reynolds number, Thermal instability, Transonic flow

Hypersonic boundary-layer transition on the BOLT forebody in the R2Ch facility.

Authors: Sombaert, Loïc Nicolas, François Lugrin, Mathieu et al.

Source: Experiments in Fluids. Jun2025, Vol. 66 Issue 6, p1-22. 22p.

Subjects: Hypersonics, Reynolds number, Aerodynamics, Turbulence, Thermography, Transition flow, Mach number