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- W783555386 abstract "An investigation has been made t o determine the aerodynamic characteristics in pitch and sideslip of a 1/15-scale model of the Scout vehicle at a Mach number of 2.01. The effects of two sets of cruciform fins, of inline and indexed fin arrangements, a flare , and accessories such as antennas, launch fittings, and control tunnels were measured for combined angles of attack and sideslip to about 8deg. The tests were made in the Langley 4- by 4-foot supersonic pressure tunnel at a Reynolds number of 4 x 10(exp 6) per foot. The Addition of the rear fins or the flare increased the longitudinal and directional stability, whereas the front fins, either indexed or inline, had a destabilizing effect. All configurations became directionally unstable with increasing angle of attack. The accessories had only a small effect on the aerodynamic characteristics other than an increase in axial force." @default.
- W783555386 created "2016-06-24" @default.
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- W783555386 date "1961-05-01" @default.
- W783555386 modified "2023-09-27" @default.
- W783555386 title "Aerodynamic Characteristics in Pitch and Sideslip of a 1/15-Scale Model of the Scout Vehicle at a Mach Number of 2.01" @default.
- W783555386 hasPublicationYear "1961" @default.
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