Pages that link to "Item:Q1146580"
From MaRDI portal
The following pages link to Laminar boundary layer on swept-back wings of infinite span at an angle of attack (Q1146580):
Displaying 8 items.
- What makes the difference between shock boundary-layer interaction on an airfoil and on a swept wing? (Q684888) (← links)
- Investigation of three-dimensional boundary layers on blunt bodies with permeable surface (Q794858) (← links)
- Laminar boundary layer on a partly moving surface in the presence of blowing or suction (Q1146579) (← links)
- Supersonic laminar flow on the windward surface of yawed wings of infinite span over a broad range of Reynolds numbers (Q1190905) (← links)
- Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow (Q1815156) (← links)
- Analysis of the three-dimensional turbulent boundary layer on the surface of an arbitrary body at large angles of attack (Q1925233) (← links)
- Distinctive features of flow in the hypersonic boundary layer in the vicinity of the plane of symmetry of a planar wing having a bend of the leading edge (Q2281952) (← links)
- (Q3771853) (← links)
