The boundary layer in hypersonic regimes—typically defined by free-stream Mach numbers exceeding five—exhibits a complex interplay of compressibility, high thermal gradients and non-equilibrium ...
The boundary layer in high Reynolds number flows is a thin region adjacent to solid surfaces where viscous forces and shear dominate despite the overwhelming inertia of the external stream. At ...
Some results have been hidden because they may be inaccessible to you
Show inaccessible results