Pages that link to "Item:Q800158"
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The following pages link to Numerical investigation of the hypersonic viscous shock layer on wings of infinite span at angles of attack and slip (Q800158):
Displaying 6 items.
- Numerical study of attack angle characteristics for integrated hypersonic vehicle (Q735307) (← links)
- 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) (← links)
- On the theory of a three-dimensional, viscous hypersonic shock layer in the neighbourhood of the plane of symmetry (Q1072861) (← links)
- Investigation of a three-dimensional hypersonic viscous shock layer on blunt bodies around which flow occurs at angles of attack and slippage (Q1089212) (← links)
- Investigation on the flow past wings of infinite span with a blunt leading edge in the vorticity interaction regime (Q1108871) (← links)
- Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow (Q1815156) (← links)
