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- W2071036989 abstract "A critical comparison has been made between the drag characteristics of a number of the best available axisymmetric body shapes using a numerical drag calculation scheme. Assuming a turbulent boundary layer over most of the body surface at Rv = 10 , the study shows that all profiles have almost equal drag coefficients when referenced to the two-third power of the body volume. However, based on the projected area, several laminar bodies were found to have substantially lower drag coefficients. Transition studies indicate that a short run of laminar boundary-layer flow, XIL to about 0.2, may be expected by moving the maximum thickness forward and carefully designing the nose shape through the inverse method. At Rv = 5 x 10, all bodies, with the exception of the Shark and F-57, have the same transition and drag characteristics. The study also shows that the F-57 shape has a much higher transition risk than the Shark in the range 0 . 0 8 < X / L < 0 . 1 3 . Otherwise, the F-57 shape has better performance. Increasing the flow acceleration in this range is expected to eliminate the transition possibility and the superiority of the F-57 profile becomes undisputed." @default.
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- W2071036989 date "1979-04-01" @default.
- W2071036989 modified "2023-09-27" @default.
- W2071036989 title "Viscious Drag Computation for Axisymmetric Bodies at High Reynolds Numbers" @default.
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- W2071036989 doi "https://doi.org/10.2514/3.63153" @default.
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