Pages that link to "Item:Q811248"
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The following pages link to A comparison of the models of a thin and a complete viscous shock layer in the problem of the supersonic flow of a viscous gas past blunt cones (Q811248):
Displaying 6 items.
- Supersonic laminar flow on the windward surface of yawed wings of infinite span over a broad range of Reynolds numbers (Q1190905) (← links)
- Viscous shock layer on a plate in hypersonic flow (Q1302521) (← links)
- Comparison of gas-dynamic models for hypersonic flow past bodies (Q1315569) (← links)
- Influence of second-order boundary layer effects in hypersonic flow over slender blunt cones (Q1317754) (← links)
- Modeling flow in a shock viscous layer (Q1735332) (← links)
- Numerical simulation of hypersonic flow around a sharp cone (Q2760774) (← links)