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- W2079274173 abstract "|UASI-steady techniques are used in a preliminary, order of magnitude, analysis of the aeroelastic stability of the space shuttle ascent configuration. The analysis shows that interference effects will result in negative aerodynamic damping of one or more of the low frequency free-free elastic modes. The implication of these results, i.e., the possibility of undamped, divergent, oscillations leading to structural failure is serious enough to warrant further analytic and experimental investigations. Since the quasi-steady technique evaluates the effect of each component of the aerodynamic load distribution on the aerodynamic damping of the elastic modes, the loads responsible for adverse dynamic effects are revealed. Thus, the analysis shows that booster-plume-induced separation and orbiter bow shock impingement on the booster are two possible sources of modal undamping." @default.
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- W2079274173 modified "2023-09-23" @default.
- W2079274173 title "Importance of Unsteady Aerodynamics for Space Shuttle Ascent Aeroelastic Stability" @default.
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- W2079274173 doi "https://doi.org/10.2514/3.56957" @default.
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