Andere Kunden interessierten sich auch für
![Structural Stability of a Joined-Wing Sensorcraft]( "Structural Stability of a Joined-Wing Sensorcraft")
Structural Stability of a Joined-Wing Sensorcraft63,99 €![Conceptual Design Oriented Wing Structural Analysis and Optimization]( "Conceptual Design Oriented Wing Structural Analysis and Optimization")
Conceptual Design Oriented Wing Structural Analysis and Optimization60,99 €![Integrated Conceptual Design of Joined-Wing Sensorcraft Using Response Surface Models]( "Integrated Conceptual Design of Joined-Wing Sensorcraft Using Response Surface Models")
Integrated Conceptual Design of Joined-Wing Sensorcraft Using Response Surface Models60,99 €![An Analysis of Nonlinear Elastic Deformations for a Homogeneous Beam at Varying Tip Loads and Pitch Angles]( "An Analysis of Nonlinear Elastic Deformations for a Homogeneous Beam at Varying Tip Loads and Pitch Angles")
An Analysis of Nonlinear Elastic Deformations for a Homogeneous Beam at Varying Tip Loads and Pitch Angles63,99 €![A Static Aeroelastic Analysis of a Flexible Wing Mini Unmanned Aerial Vehicle]( "A Static Aeroelastic Analysis of a Flexible Wing Mini Unmanned Aerial Vehicle")
A Static Aeroelastic Analysis of a Flexible Wing Mini Unmanned Aerial Vehicle63,99 €![Wind Tunnel Ivestigation of Joined Wing Configurations]( "Wind Tunnel Ivestigation of Joined Wing Configurations")
Wind Tunnel Ivestigation of Joined Wing Configurations60,99 €![A Wind Tunnel Investigation of Joined Wing Scissor Morphing]( "A Wind Tunnel Investigation of Joined Wing Scissor Morphing")
A Wind Tunnel Investigation of Joined Wing Scissor Morphing61,99 €
This study is based on the merger of two separate theories to further the efficiency with which joined-wing structural models are designed. The first theory is Geometrically Exact Beam Theory (GEBT). GEBT is a small strain beam theory which is capable of accurately capturing the geometric bend-twist coupling in beam elements that are experiencing large global deformations. This is crucial to the joined-wing problem as it is geometrically nonlinear. The second theory concerns Equivalent Static Loads (ESL). These ESL consist of a load vector that produces the same nodal displacements and rotations as those computed from a pure nonlinear analysis. The ESL displacements and rotations are then used to calculate ESL stresses. By merging these two theories into a single structural optimization effort, computational cost is reduced by orders of magnitude when compared to purely nonlinear response optimization efforts. It is shown that the final design obtained by the optimization is the same for both types of analysis.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.