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Hypersonic flow around two cylinders
Hypersonic flow around two cylinders
D
29 August 2009
Case description
inviscid flow
upstream Mach number 10
Numerical Parameters
first order HLLC scheme
Results
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Pages
Unsteady shock Wave / boundary Layer interaction
Multi-element inviscid flow (Suddhoo-Hall)
Shock reflection/diffraction over pyramid
Supersonic reflexion on 10° wedge
Unsteady Supersonic flow over parabolic 20% bump