Pages that link to "Item:Q1190905"
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The following pages link to Supersonic laminar flow on the windward surface of yawed wings of infinite span over a broad range of Reynolds numbers (Q1190905):
Displaying 3 items.
- Behaviour of a rectangular wing in a supersonic flow-dynamic pressure and normal force analysis in the range 1.3-4.0 mach (Q1065639) (← links)
- Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow (Q1815156) (← links)
- Supercritical regimes of hypersonic flow past a planar yawed delta wing (Q1925267) (← links)