Explicit analytic solution for similarity boundary layer equations

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Series Solutions of Unsteady Boundary‐Layer Flows over a Stretching Flat Plate (2006, methodology): “Using the asymptotic property (12) of the steady-state solution (see Liao and Pop [23]), we λ = δs/2, (71) where δs = δ(1) is defined by (13) and is known from Liao and Pop’s work [23] for the corresponding steady-state problem.”
A general approach to get series solution of non-similarity boundary-layer flows (2009, methodology): “It is interesting that Liao and Pop [43] used the same auxiliary linear operator to solve similarity boundary-layer flows.”
A unified gas-kinetic scheme for continuum and rarefied flows,direct modeling,and full Boltzmann collision term (2014, unknown): “ity, U, and V velocity contours are shown in Fig.(23(b))-(23(d)). The U and V velocity proles at dierent locations are plotted in Fig.(24), where the solid lines are the reference Blasius solutions [28]. Even with as less as 5 mesh points in the boundary layer, both Uand V velocity components can be”
A new branch of solutions of boundary-layer flows over an impermeable stretched plate (2005, methodology): “So, different from Banks [3] and Liao and Pop [15], we successfully find the two branches of solutions”