Pages that link to "Item:Q1317696"
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The following pages link to 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):
Displaying 5 items.
- Numerical modeling of the effect of geometric asymmetry on the damping aerodynamic characteristics of supersonic sectional flight vehicles (Q604616) (← links)
- Supersonic laminar flow on the windward surface of yawed wings of infinite span over a broad range of Reynolds numbers (Q1190905) (← links)
- Numerical study of steady supersonic separated flow past spatial lifting systems (Q1316781) (← links)
- Numerical solution for complete aircraft's subsonic-transonic-supersonic flow at high angles of attack (Q1388008) (← links)
- Information technology of mathematical modelling of a three-dimensional supersonic flow on the basis of particular solutions of hydrodynamic problems (Q4354669) (← links)