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- W2005356186 abstract "Measured shock shapes are presented for sphere and hemisphere models in helium, air, CF4, C2F6, and CO2 test gases, corresponding to normal-shock density ratios (primary factor governing shock detachment distance of blunt bodies at hypersonic speeds) from 4 to 19. These shock shapes were obtained in three facilities capable of generating the high density ratios experienced during planetary entry at hypersonic conditions; namely, the 6-inch expansion tube, with hypersonic CF4 tunnel, and pilot CF4 Mach 6 tunnel (with CF4 replaced by C2F6). Measured results are compared with several inviscid perfect-gas shock shape predictions, in which an effective ratio of specific heats is used as input, and with real-gas predictions which include effects of a laminar viscous layer and thermochemical nonequilibrium." @default.
- W2005356186 created "2016-06-24" @default.
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- W2005356186 date "1975-12-01" @default.
- W2005356186 modified "2023-09-26" @default.
- W2005356186 title "A comparison of measured and predicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19" @default.
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