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- W613150257 abstract "The effect of forebody geometry on the stability of the laminar boundary layer on axisymmetric body shapes at Reynolds numbers typical of small and medium sized aircraft in low-subsonic cruise flight is investigated. It is found that small nose radii are important in obtaining n-factors of 9 on axisymmetric bodies of fineness ratio of about 6 at large nondimensional axial distances downstream. Results for the effect of the steepness of the pressure gradient and the value of the minimum pressure on the extent of laminar flows on an axisymmetric body at a given Reynolds number are also presented." @default.
- W613150257 created "2016-06-24" @default.
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- W613150257 date "1987-01-01" @default.
- W613150257 modified "2023-09-27" @default.
- W613150257 title "Effects of forebody geometry on subsonic laminar boundary layer stability" @default.
- W613150257 hasPublicationYear "1987" @default.
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