Pages that link to "Item:Q802409"
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The following pages link to Investigation of hypersonic flow of rarefied gas past wings of infinite span (Q802409):
Displaying 4 items.
- Numerical investigation of the hypersonic viscous shock layer on wings of infinite span at angles of attack and slip (Q800158) (← links)
- Investigation on the flow past wings of infinite span with a blunt leading edge in the vorticity interaction regime (Q1108871) (← links)
- Laminar boundary layer on swept-back wings of infinite span at an angle of attack (Q1146580) (← links)
- Supersonic laminar flow on the windward surface of yawed wings of infinite span over a broad range of Reynolds numbers (Q1190905) (← links)