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- W1506069200 abstract "Report presenting testing of a fineness-ratio-2.71 right circular cylinder and a fineness-ratio-4.0 circular cylinder with a rounded nose and flared afterbody over a range of Mach and Reynolds numbers. Time histories, cross plots of force coefficients, rolling velocity, and longitudinal-force coefficient are provided for the two cylinders." @default.
- W1506069200 created "2016-06-24" @default.
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- W1506069200 date "1958-03-18" @default.
- W1506069200 modified "2023-09-26" @default.
- W1506069200 title "Investigation of Two Bluff Shapes in Axial Free Flight over a Mach Number Range from 0.35 and 2.15" @default.
- W1506069200 cites W2161717505 @default.
- W1506069200 hasPublicationYear "1958" @default.
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