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- W86131095 abstract "An experimental aerodynamic investigation was conducted on a 0.01 scale model of a Langley concept space shuttle orbiter (LO-100) in the Langley Low Turbulence Pressure Tunnel at a Mach number of 0.25 and at a Reynolds number of 5.4 million per foot. The angle of attack was varied from about -2 deg to 24 deg at 0 deg and 5 deg sideslip. The configuration was tested at elevon settings of 0 deg, -5 deg, -10 deg, and -15 deg for a body base flap setting of 0 deg and at 0 deg, -10 deg, and -15 deg for a body base flap setting of -18 deg. The effect of rudder flare angle was obtained using 0 deg, 20 deg, and 40 deg, flare settings." @default.
- W86131095 created "2016-06-24" @default.
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- W86131095 date "1973-10-01" @default.
- W86131095 modified "2023-09-26" @default.
- W86131095 title "Stability and control characteristics of a Langley concept space shuttle orbiter (LO-100) at low subsonic speeds" @default.
- W86131095 hasPublicationYear "1973" @default.
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