Pages that link to "Item:Q633508"
From MaRDI portal
The following pages link to Shock layers over blunt and conical bodies in hypersonic non-equilibrium flow (Q633508):
Displaying 11 items.
- Experimental investigation of flow past simple model bodies in hypersonic wind tunnels at similar values of the Mach and Reynolds numbers but at different physical flow velocities (Q893521) (← links)
- Nonequilibrium excitation of internal molecular degrees of freedom in the shock layer during hypersonic flight (Q1202416) (← links)
- Comparison of gas-dynamic models for hypersonic flow past bodies (Q1315569) (← links)
- A thermally non-equilibrium viscous shock layer past slender blunted cones (Q1359905) (← links)
- Comparison of the calculated results for hypersonic flow past blunt bodies with the OREX flight test data (Q1402833) (← links)
- Comparison of different approaches to the calculation of chemically nonequilibrium flow with allowance for vibrational relaxation (Q1815108) (← links)
- Conical flow breakdown in non-free shock-wave/boundary-layer interaction (Q2269404) (← links)
- Inviscid vortex structures in the shock layers of conical flows around V wings (Q2402756) (← links)
- (Q4829091) (← links)
- Hypersonic flow over spherically blunted cone capsules for atmospheric entry. Part 1. The sharp cone and the sphere (Q5382899) (← links)
- Hypersonic flow over spherically blunted cone capsules for atmospheric entry. Part 2. Vibrational non-equilibrium effects (Q5870475) (← links)
