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 ...
Your institution does not have access to this book on JSTOR. Try searching on JSTOR for other items related to this book. The Navier-Stokes Equations for a Viscous Heat-Conducting Compressible Fluid ...
Some results have been hidden because they may be inaccessible to you
Show inaccessible results