Plate Bending Introduction see: bending with z load sheet for derivations review general beam, simply supported, clamped long plate long plate, boundary conditions (end restrained) not so long plate simply supported beam: w q⋅b b Q( x) := 2 M ⋅x − q⋅ x⋅ b → 2 σ x := t b x q⋅bb a − q⋅ x 2 ⌠ 1 1 2 Q( ξ ) dξ → ⋅q⋅b⋅x − ⋅q⋅x ⌡ 2 2 0 M ( x) := t q x M ( x) I 1 8 z x 1 d M ( x) → ⋅q⋅b − q⋅ x 2 dx 2 1 M max := 2 ⋅q⋅b 8 = 0 @ x = b/2 2 ⋅q⋅bb σ x_max := maximum when z = t/2, m(x) = Mmax ⋅z 1 2 ⋅q⋅b M max t ⋅ I 2 + tension other side of load 2 3 b 8 1 3 t ⋅t ⋅aa σ x_max := ⋅ σ x_max → ⋅q⋅ - compression on load side I 2 2 4 12 t ⋅a ___________________________________________________________________________________________ I := clamped beam: need to use delection x 4 w d q t a w to solve 4 dx x2 M ( x) := −q⋅ result: Given d M ( x) = 0 dx 2 − bb⋅ x 2 + 2 b b 12 Find( x) → 1 2 z ⋅b M b 2 → σ x_max := 1 12 2 ⋅q⋅b I ⋅ t 2 24 2 ⋅ q⋅b M ( 0) → M max = M ( x = 0, x = b) 1 1 σ x_max → 1 2 2 ⋅q⋅ b 2 t ⋅a −1 12 2 ⋅ q⋅b M ( b) → −1 12 - compression other side of load + tension on load side notes_22_plate_bending_intro.mcd 2 ⋅ q⋅b t long plate: treating unit length (away from end effects) t b x a a := 1 w(x) y section at a simply supported free to pull in z t q x w a t da t b z strain in y constrained by adjacent plate anticlastic curvature Rν = 1/ν ∗ R ε x := σx E − ν ⋅σ y E ε y := (1 − ν )⋅σσ x σy E 2 substituting => ε x:= rearranging => σ x := or ... ε x:= E E⋅ε x σx E' 2 ν ⋅σ x E where E' = E/(1-ν^2) ε x := − z => R E σ x := − 1− ν E⋅tt D := 2 3 2 d M := −D⋅ 2 12⋅ ( 1 − ν ) 8 I ⋅ t 2 ⋅ d 2 M = My w dxx w σ x_max := 3 4 1 2 ⋅q⋅ b t σ x_max := 2 2 Hughes 9.1.7 is of the form: 12⋅ ( 1 − ν ) 2 2 clamped: (figure not shown) 2 ⋅q⋅b 3 dx x moment relationships are the same: simply supported: 1 2 M := − E⋅ t σ x_max := k⋅ q⋅ b t 2 12 2 ⋅q⋅b I ⋅ t 2 σ x_max := k = 0.75 simply supported k = 0.5 clamped N.B. stress is + & - from bending notes_22_plate_bending_intro.mcd 1 2 2 ⋅q⋅ b t 2 ⋅ z 2 R t ⌠2 2 E⋅ z d w⋅z dz M := − ⋅ 2 dx2 1− ν − t ⌡ 2 2 = as in bending of beam: t ⌠2 M := σ x⋅z dz ⌡− t σ x_max := E ( 1−ν 2) 1− ν define: σy =0 E σx or ... ε x:= E ν ⋅σ σx −