AA SEZC method 7.3.2 bending stiffness
3
Abbott Aerospace – Analysis Method XL-VIKING Display Your Math in Excel Taken from: Analysis and Design of Composite and Metallic Flight Vehicle Structures Bending Stiffness
-
Upload
richard-abbott -
Category
Engineering
-
view
110 -
download
5
Transcript of AA SEZC method 7.3.2 bending stiffness
Abbott Aerospace – Analysis Method
XL-VIKINGDisplay Your Math in Excel
Taken from: Analysis and Design of Composite and Metallic Flight Vehicle Structures
Bending Stiffness
Abbott Aerospace – Analysis Method
XL-VIKINGDisplay Your Math in Excel
Taken from: Analysis and Design of Composite and Metallic Flight Vehicle Structures
Bending Stiffness
Simple Cantilever
The expression will be given in terms of stiffness per unit width
𝛿 =4 ∙ 𝑃 ∙ 𝐿3
𝐸 ∙ 𝑡3
Where:𝜹 Deflection in the direction of the force vector, in𝑷 Force applied, lb𝑳 Original length of the cantilever beam, in𝑬 Young’s modulus of the member material, psi𝒕 Thickness of the beam, in
The expression for Stiffness can easily be derived as
𝑘 =𝐸 ∙ 𝑡3
4 ∙ 𝐿3
Abbott Aerospace – Analysis Method
XL-VIKINGDisplay Your Math in Excel
Taken from: Analysis and Design of Composite and Metallic Flight Vehicle Structures
Bending Stiffness
Guided Cantilever
The expression will be given in terms of stiffness per unit width:
𝛿 =𝑃 ∙ 𝐿3
𝐸 ∙ 𝑡3
The expression for Stiffness can easily be derived as
𝑘 =𝐸 ∙ 𝑡3
𝐿3
AA-SM-260 Tools - Spring Stiffness of Cantilever Beams
