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- W844416883 abstract "Results have been obtained i n t h e Langley 8-foot transonic pressure tunnel at Mach numbers from 0.40 t o 1.20 for several configurations of the Scout vehicle and f o r a number of related models. Tests extended over an angle-of-attack range from about -10 degrees to 10 degrees at a Reynolds number per foot of about 3.8 x 10 sup 6." @default.
- W844416883 created "2016-06-24" @default.
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- W844416883 date "1961-05-01" @default.
- W844416883 modified "2023-09-23" @default.
- W844416883 title "Transonic Wind-Tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Configurations of the Scout Vehicle and of a Number of Related Models" @default.
- W844416883 hasPublicationYear "1961" @default.
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