Laminar Boundary Layer Behind Shock Advancing into Stationary Fluid. Mirels, H. Technical Report 3401, National Advisory Committee for Aeronautics, 1955.
bibtex   
@techreport{mirels1955,
	title = {Laminar {Boundary} {Layer} {Behind} {Shock} {Advancing} into {Stationary} {Fluid}},
	number = {3401},
	institution = {National Advisory Committee for Aeronautics},
	author = {Mirels, Harold},
	year = {1955},
}

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