Kód: 08243215
This study developed a multi-disciplinary conceptual design of a joined-wing sensor-craft. Initial analysis was conducted using an aluminum model. Linear fully stressed design and flexible aerodynamic trim were used to converge to ... celý popis
Angličtina
Nákupem získáte 42 bodů
Anotace knihy
This study developed a multi-disciplinary conceptual design of a joined-wing sensor-craft. Initial analysis was conducted using an aluminum model. Linear fully stressed design and flexible aerodynamic trim were used to converge to a minimum weight design that was aerodynamically stable. This optimized design was buckling safe. A similar optimization process using non-linear fully stressed design and flexible aerodynamic trim was conducted. The non-linear structural deformation was over ten times greater than the linear structural deformation. Again, the model was structurally and aerodynamically optimized. The linear optimization was repeated using a composite structural model incorporating Conformal Load-bearing Antenna Structures. This research demonstrated the importance of considering non-linearity and the coupling of aerodynamic and structural design.
Parametry knihy
Zařazení knihy Knihy v angličtině Society & social sciences Education
423 Kč
Angličtina
Osobní odběr Praha, Brno a 47484 dalších
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