Pages that link to "Item:Q1815156"
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The following pages link to Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow (Q1815156):
Displaying 4 items.
- Laminar boundary layer on swept-back wings of infinite span at an angle of attack (Q1146580) (← links)
- Heat transfer in the neighborhood of a point of injection in the leading edge of a plate in hypersonic flight (Q1149333) (← links)
- Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies (Q1676232) (← links)
- Heat transfer on yawed infinite cylinders in a hypersonic stream (Q1925252) (← links)