Pages that link to "Item:Q1676232"
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The following pages link to Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies (Q1676232):
Displaying 12 items.
- Approximate formulas for heat flows towards an ideally catalytic surface near a plane of symmetry (Q811288) (← links)
- Three-dimensional thermal boundary layer corrections for circular heat flux gauges mounted in a flat plate with a surface temperature discontinuity (Q865875) (← links)
- Heat transfer at the surface of a triangular body in a hypersonic viscous gas flow (Q1115724) (← links)
- A review of semi-analytical solutions for flame impingement heat transfer (Q1297306) (← links)
- Extremal problems of heat transfer to three-dimensional bodies at hypersonic speeds (Q1314204) (← links)
- Approximate formulas for the heat fluxes to the surface of three- dimensional bodies (Q1314205) (← links)
- Comparison of approximate analytical and numerical solutions for heat fluxes in viscous supersonic flow past a body (Q1354791) (← links)
- Heat transfer to blunt-edged swept wings at angle of attack in hypersonic flow (Q1815156) (← links)
- Approximation formulas for the radiative heat flux at high velocities (Q2281963) (← links)
- A kinetic shock layer in the spreading plane of a lifting-body apparatus (Q2668104) (← links)
- Кинетический вязкий ударный слой вблизи передней кромки тонкого вращающегося диска;Kinetyc viscous shock layer near leading edge of a thin rotating disc (Q6143328) (← links)
- Hypersonic nonequilibrium flow around a sharp edge (Q6563543) (← links)
