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- W339909141 abstract "Abstract : Methods and procedures were developed for extrapolating ground-test aerothermodynamic data to flight conditions for four geometric elements. These elements are a sharp unyawed delta wing, deflected control surfaces in compression and expansion, surface roughness elements typified by shallow convex surface waves and rectangular grooves, and a yawed circular cylinder intersecting a sharp flat plate. Graphs and charts are provided for rapid numerical computation of factors to be used in extrapolating the wind-tunnel data for these geometric elements to flight conditions. An evaluation of the simulation capabilities of operational hypersonic ground facilities is also included." @default.
- W339909141 created "2016-06-24" @default.
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- W339909141 date "1967-01-01" @default.
- W339909141 modified "2023-09-22" @default.
- W339909141 title "APPLICATION OF GROUND TEST DATA TO REENTRY VEHICLE DESIGN" @default.
- W339909141 doi "https://doi.org/10.21236/ad0655383" @default.
- W339909141 hasPublicationYear "1967" @default.
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