Pages that link to "Item:Q1316781"
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The following pages link to Numerical study of steady supersonic separated flow past spatial lifting systems (Q1316781):
Displaying 3 items.
- Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections (Q1317696) (← links)
- Development of wave potential theory in time-dependent problems of supersonic separated flow around three-dimensional lifting systems (Q1390559) (← links)
- Numerical simulation of the lateral aerodynamics of an orbital stage at stage separation flow conditions (Q4500545) (← links)