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- W147538315 abstract "The Langley 8 foot transonic pressure tunnel and the Langley Unitary Plan wind tunnel used to determine the longitudinal and lateral-directional aerodynamic characteristics of a winged single-state-to-orbit vehicle was investigated. The model was tested over a Mach number range from 0.3 to 4.63 for an angle-of-attack range from 4 to 30 D at both 0 and 5 D sideslip." @default.
- W147538315 created "2016-06-24" @default.
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- W147538315 date "1978-08-01" @default.
- W147538315 modified "2023-09-27" @default.
- W147538315 title "Static aerodynamic characteristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63" @default.
- W147538315 hasPublicationYear "1978" @default.
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