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- W851897581 abstract "The purpose of this study was to determine the hypersonic aerodynamic performance, longitudinal trim, static stability, and the extent of the center-of-gravity boundaries within the design control limits as well as to examine the effect of Reynolds number on the longitudinal stability of the 139-B space shuttle orbiter. A 0.004 scale model (34-0)was tested in helium over an angle-of-attack range of 18 deg to 54 deg at 0 deg and -minus 5 deg sideslip angles. The total pressure was varied for selected configurations to obtain a Reynolds number range, based on model length, from 0.51 million to 3.6 million at Mach numbers between 17.6 and 21.6 Surface oil-flow studies and electron-beam illuminated-flow studies were also conducted at angles-of-attack of 30 deg, 40 deg, and 50 deg for selected Reynolds numbers." @default.
- W851897581 created "2016-06-24" @default.
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- W851897581 date "1974-07-01" @default.
- W851897581 modified "2023-09-27" @default.
- W851897581 title "Hypersonic stability and control characteristics of the Rockwell International 139-B space shuttle orbiter" @default.
- W851897581 hasPublicationYear "1974" @default.
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