The report contains abstracts of significant research papers developed on the laminar compressible boundary layer in the stagnation-point region for an axisymmetric blunt body, second-order boundary layer effects in hypersonic flow past axisymmetric blunt bodies, two-dimensional hypersonic stagnation flow at low Reynolds numbers, and a numerical solution for the laminar wake behind a finite flat plate. (Author).

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.