NASA NTRS · 19760011965
FLEXSTAB analysis
Abstract
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 flight and analytical data of wing pressure distributions and static longitudinal stability derivatives.
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Lowder, H. E., Jr.. 1976-02-01. FLEXSTAB analysis. https://ntrs.nasa.gov/citations/19760011965
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