Pages that link to "Item:Q1625635"
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The following pages link to An effective flux scheme for hypersonic heating prediction of re-entry vehicles (Q1625635):
Displaying 8 items.
- Comparisons and applications of numerical simulation methods for predicting aerodynamic heating around complex configurations (Q362886) (← links)
- A method for calculating intense injection from surfaces of blunt bodies entering planetary atmospheres at hypersonic velocities (Q604580) (← links)
- A unified construction of all-speed HLL-type schemes for hypersonic heating computations (Q2072346) (← links)
- (Q3160177) (← links)
- Considerations on CFD modeling for the design of re-entry vehicles (Q4524941) (← links)
- Numerical study of instabilities and compressibility effects on supersonic jet over a convex wall (Q5872981) (← links)
- Mixing enhancement of a compressible jet over a convex wall (Q6081836) (← links)
- Unified stochastic particle simulation of polyatomic gas flows using SPARTACUS (Q6095906) (← links)