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- W2146521343 abstract "This research performs aeroelastic analysis of a clamped, thin-film ballute on a Titan aerocapture trajectory of suitable fidelity for conceptual design work. Static deformed shapes and stresses are computed along a Titan Aerocapture trajectory, and an engineering estimate of unsteady hypersonic flow is used to determine if the ballute flutters at the peak dynamic pressure point. Static solutions along a Titan aerocapture trajectory indicate that stress and displacement are correlated to dynamic pressure above 1 Pa. For lower dynamic pressures, the aerodynamic loading is insucient to fully overcome initial material shape, indicating that spacecraft re-contact is possible, and leading to a recommendation to include supports for the torus. Dynamic analysis of the clamped ballute using a first-order engineering estimate of unsteady aerodynamics indicates that flutter will not be a problem at the peak dynamic pressure point on the trajectory." @default.
- W2146521343 created "2016-06-24" @default.
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- W2146521343 date "2007-04-23" @default.
- W2146521343 modified "2023-09-23" @default.
- W2146521343 title "Aeroelastic Design Considerations of a Clamped Ballute for Titan Aerocapture" @default.
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- W2146521343 doi "https://doi.org/10.2514/6.2007-1850" @default.
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