Boundary Layer Behind Shock or Thin Expansion Wave Moving into Stationary Fluid. Mirels, H. Technical Report 3712, National Advisory Committee for Aeronautics, 1956. bibtex @techreport{mirels1956,
title = {Boundary {Layer} {Behind} {Shock} or {Thin} {Expansion} {Wave} {Moving} into {Stationary} {Fluid}},
number = {3712},
institution = {National Advisory Committee for Aeronautics},
author = {Mirels, Harold},
year = {1956},
}
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