NASA Technical Reports Server (NTRS) 19760011965: FLEXSTAB analysisReportar como inadecuado




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The wing differential pressure distributions of two vehicles are predicted using FLEXSTAB. Three space shuttle configurations were investigated. Comparisons were made of wind tunnel and analytical data for a selected range of angle of attack, angle of sideslip, and Mach number. A drone-type vehicle was investigated and comparisons were made between

Autor: NASA Technical Reports Server (NTRS)

Fuente: https://archive.org/







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