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Load State of an Aircraft with an Elastic Wing
Schoř, Pavel ; Daněk, Vladimír (oponent) ; Slavík, Svatomír (oponent) ; Píštěk, Antonín (vedoucí práce)
This thesis proposes a methodology, how to calculate the load state of an aircraft with an elastic wing by first-order panel panel method according to Katz and Plotkin, Low-Speed Aerodynamics, 2001 coupled to a struc- tural analysis method according to Píštěk et al., Pevnost a životnost letadel I, 1988 and Lebofsky,Numerically Generated Tangent Stiffness Matrices for Geometrically Non-Linear Structures, 2013. For a flow, which is similar to a potential flow, panel methods can provide an accurate information about all characteristics required for a calculation of aerodynamic load. Unlike the CFD based methods, this method can be used on an average personal computer.
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Load State of an Aircraft with an Elastic Wing
Schoř, Pavel ; Daněk, Vladimír (oponent) ; Slavík, Svatomír (oponent) ; Píštěk, Antonín (vedoucí práce)
This thesis proposes a methodology, how to calculate the load state of an aircraft with an elastic wing by first-order panel panel method according to Katz and Plotkin, Low-Speed Aerodynamics, 2001 coupled to a struc- tural analysis method according to Píštěk et al., Pevnost a životnost letadel I, 1988 and Lebofsky,Numerically Generated Tangent Stiffness Matrices for Geometrically Non-Linear Structures, 2013. For a flow, which is similar to a potential flow, panel methods can provide an accurate information about all characteristics required for a calculation of aerodynamic load. Unlike the CFD based methods, this method can be used on an average personal computer.
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