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Continuum Mechanics Cheat Sheet, Cheat Sheet of Mechanics

Cheat sheet of Continuum Mechanics on: Spectral theorem, Navier-Stokes equations in polar coordinates, Ideal gas computatio

Typology: Cheat Sheet

2019/2020

Uploaded on 10/09/2020

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MAT252 cheat sheet
(continuum mechanics)
Tommy Odland
Spectral theorem
Summation bi=Pjaijxj=aij xjdiv(v) = vi,i = vi
∂xi=∂v1
∂x1+∂v2
∂x2+...
Symmetry The matrix Mis symmetric if MT=M. If MT=M,the matrix
is antisymmetric. Every matrix Mcan be expressed as:
M=A+S=1
2MMT
| {z }
antisymmetric
+1
2M+MT
| {z }
symmetric
Gram-Schmidt Given vectors {u1,u2, ...., un}, do:
u1:= u1/||u1||
u2:= u2(u2·u1)u1
u2:= u2/||u2||
u3:= u3(u3·u1)u1(u3·u2)u2
u3:= u3/||u3||
un:= unPi(un·ui)ui
To create a set in Rn, start with u1and require that uibe orthogonal
to all previous by solving system with (i1) unknowns.
Navier-Stokes equations in polar coordinates
Gradient The gradient is grad v=v
∂xjej=(viei)
∂xjej
Divergence The divergence is div v=v
∂xj·ej=(viei)
∂xj·ej.
Digergence of tensor div T=T
∂xk·ek=
∂xk[Tij (eiej)] ·ek
Tensor rule (ab)c=a(b·c)
Navier-Stokes ρDu
Dt = · σ+ρfma=PiFi
Euler ρDu
Dt =∇·−pI(No viscosity)
Material derivative D
Dt
∂t +u·
Polar coordinates and solid-body rotation
Solid body rotation The solid body rotation is v(r, θ) = (vr, vθ) = (0, ωr)in polar
coordinates and v(x, y)=(vx, vy) = ω(y, x)in Cartesian
Lagrangian variables in two dimensions
Strain rate tensor Let vbe a velocity field (deformation mapping), the strain rate
tensor is: dij =1
2(di,j +dj,i)
Change of v
v=d
|{z}
strain rate
+w
|{z}
rotation
=df
|{z}
pure strain
+de
|{z}
expansion
+w
|{z}
rotation
where de=1
3tr dand df= (dde).
Ideal gas computations
Ideal gas law The ideal gas law is P V =nRT , where nis moles
and Ris a gas constant.
First law of thermodynamics The 1st law is dU =dqdw, where Uis the internal
energy of the fluid, qis heat into fluid and wis work
onto environment.
Entropy Entropy Sis given by dS =dq
T
Exact differential dQ is exact Qis a state function HdQ = 0
Second law of thermodynamics
Carnot engine (1) Isothermal expansion, (2) Adiabatic expansion, (3) Isother-
mal compression, (4) Adiabatic expansion. Isothermal means
constant temperature, adiabatic means no heat transfer.
Efficiency of CE Efficiency is given by η=Wout
Qin = 1 TL
TH
pf2

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MAT252 cheat sheet

(continuum mechanics)

Tommy Odland

Spectral theorem

Summation b i =

j a ij^ x j^ =^ a ij^ x j^ div( v ) =^ v i,i^ =^

∂vi ∂xi =^

∂v 1 ∂x 1 +^

∂v 2 ∂x 2 +^ ...

Symmetry The matrix M is symmetric if M T^ = M. If M T^ = −M ,the matrix is antisymmetric. Every matrix M can be expressed as:

M = A + S =

M − M T^

antisymmetric

M + M T^

symmetric

Gram-Schmidt Given vectors {u 1 , u 2 , ...., u n }, do: u 1 := u 1 /||u 1 || u 2 := u 2 − (u 2 · u 1 )u 1 u 2 := u 2 /||u 2 || u 3 := u 3 − (u 3 · u 1 )u 1 − (u 3 · u 2 )u 2 u 3 := u 3 /||u 3 || u n := u n

i (u n^ ·^ u i )u i To create a set in R n , start with u 1 and require that u i be orthogonal to all previous by solving system with (i − 1) unknowns.

Navier-Stokes equations in polar coordinates

Gradient The gradient is grad v = (^) ∂x∂ v je j = ( ∂xvi e j i )⊗ e j

Divergence The divergence is div v = (^) ∂x∂ v j · e j = ( ∂xvi e j ie j.

Digergence of tensor div T = (^) ∂x∂ T k · e k = (^) ∂x∂k [T ij ( e ie j )] · e k

Tensor rule (a ⊗ b)c = a(b · c)

Navier-Stokes ρ D Dt u = ∇ · σ + ρ f ⇔ m a =

i F i

Euler ρ D Dt u = ∇ · −p I (No viscosity)

Material derivative (^) DtD ≡ (^) ∂t∂ + u · ∇

Polar coordinates and solid-body rotation

Solid body rotation The solid body rotation is v(r, θ) = (v r , v θ ) = (0, ωr) in polar coordinates and v(x, y) = (v x , v y ) = ω(−y, x) in Cartesian

Lagrangian variables in two dimensions

Strain rate tensor Let v be a velocity field (deformation mapping), the strain rate tensor is: d ij = 12 (d i,j + d j,i )

Change of vv = (^) ︸︷︷︸ d strain rate

  • (^) ︸︷︷︸ w rotation

= d f ︸︷︷︸ pure strain

  • (^) ︸︷︷︸ d e expansion

  • (^) ︸︷︷︸ w rotation

where d e = 13 tr d and d f = ( dd e ).

Ideal gas computations

Ideal gas law The ideal gas law is P V = nRT , where n is moles and R is a gas constant.

First law of thermodynamics The 1st law is dU = dq −dw, where U is the internal energy of the fluid, q is heat into fluid and w is work onto environment.

Entropy Entropy S is given by dS = dqT

Exact differential dQ is exact ⇔ Q is a state function ⇔

dQ = 0

Second law of thermodynamics

Carnot engine (1) Isothermal expansion, (2) Adiabatic expansion, (3) Isother- mal compression, (4) Adiabatic expansion. Isothermal means constant temperature, adiabatic means no heat transfer.

Efficiency of CE Efficiency is given by η = W Qoutin = 1 − (^) TTLH

Carnot theorem (1) Between T H and T L , no engine beats the efficiency of the CE. (2) Efficiency η of CE is only a function of T H and T L.

Clausius postulate Heat never flows from hot to cold without aid(work input).

One-dimensional models for an elastic beam

Strain ` is the length of the bar, u(x) is displacement

ε =

∆`

` 0

du dx

Hookes law σ is stress, ε is strain, E is modulus of elasticity

σ = Eε

Wave equation ∂^2 u ∂x^2

ρ E

∂^2 u ∂t^2

Stress and displacement in a beam with longitudinal loading

Strain sdf

For general math, see [3]. For fluids, see [2]. For thermodynamics, see [4]. For solid mechanics, see [1].

References

[1] Lubliner, J., and Papadopoulos, P. Introduction to Solid Mechanics: An Integrated Approach. Springer New York: New York, NY, 2014. [2] Pijush K. Kundu. Fluid mechanics , 5th ed. ed. Academic Press Elsevier, 2012. [3] Tadmor, E. B., Miller, R. E., and Elliott, R. S. Continuum Mechanics and Ther- modynamics: From Fundamental Concepts to Governing Equations. Cambridge University Press, Cambridge, 2011. [4] Walter J. Moore. Physical chemistry , 3rd ed. ed. Prentice-Hall chemistry series. Prentice-Hall, 1962.