18 the Lax Wendroff Technique

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    The Lax-Wendroff Technique

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    Introduction What a kind of techniques is it ?

    The Lax-Wendroff techniques is an explicit,

    finite-differencemethod particularly suited to

    marchingsolutions. A brief review on the marching problems

    Hyperbolic and parabolic partial differentialequations

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    Introduction An example of hyperbolic equations

    The time-marching solution of an invicid flow using theunsteady Euler equations (2D).

    Continuity

    +

    +

    +

    =

    y

    v

    y

    v

    x

    u

    x

    u

    t

    +

    +

    =

    x

    p

    y

    vv

    x

    uu

    t

    u

    1x momentum

    y momentum

    +

    +

    =

    y

    p

    y

    vv

    x

    vu

    t

    v

    1

    Energy

    +

    +

    +

    =

    y

    vp

    x

    up

    y

    eu

    x

    e

    t

    e

    (6.1)

    (6.2)

    (6.3)

    (6.4)

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    Procedure Predict the the value of the variables at next time step

    based on a Taylor series expansion.

    Choose density for purposes of illustration

    +

    +

    +=+

    2

    )(2

    ,2

    2

    ,

    ,,

    t

    tt

    t

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    (6.5)

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    Procedure Analogous Taylor series are written for all the other

    dependent variables.

    +

    +

    +=+2

    )(2

    ,

    2

    2

    ,

    ,,

    t

    t

    ut

    t

    uuu

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    +

    +

    +=+2

    )(2

    ,

    2

    2

    ,

    ,,

    t

    t

    vt

    t

    vvv

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    +

    +

    +=+2

    )(2

    ,

    2

    2

    ,

    ,,

    t

    t

    et

    t

    eee

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    (6.6)

    (6.7)

    (6.8)

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    Procedure

    A number for (/t) is obtained from the continuityequation, Eq. (6.1)

    The spatial derivative are given by second-order

    central differences

    +

    +

    +=+2

    )(2

    ,

    2

    2

    ,

    ,,

    t

    tt

    t

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    (

    )y

    u

    y

    vv

    xu

    x

    uu

    t

    t

    ji

    t

    jit

    ji

    t

    ji

    t

    jit

    ji

    t

    ji

    t

    jitji

    t

    ji

    t

    jitji

    t

    ji

    +

    +

    +

    =

    ++

    ++

    22

    22

    ,1,1

    ,

    ,1,1

    ,

    ,1,1,

    ,1,1,

    ,

    (6.9)

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    Procedure+

    +

    +=+2

    )(2

    ,

    2

    2

    ,

    ,,

    t

    tt

    t

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    t

    v

    ytyvty

    v

    ty

    v

    t

    u

    xtxutx

    u

    tx

    u

    t

    +

    +

    +

    +

    +

    +

    +

    =

    2222

    2

    2

    The mixed derivative is found by differentiating Eq.(6.2) with

    respect to x

    xx

    p

    x

    p

    x

    v

    y

    u

    yx

    uv

    x

    u

    x

    uu

    tx

    u

    +

    +

    +

    +

    =

    22

    222

    2

    2211

    Differentiate Eq. (6.1) with respect to time

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    Procedure

    Second-order, centered finite-difference quotients at time t

    xx

    pp

    x

    ppp

    x

    vv

    y

    uu

    yx

    uuuu

    v

    x

    uu

    x

    uuuu

    tx

    u

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    ji

    t

    jit

    ji

    tji

    tji

    tji

    tji

    tjit

    ji

    t

    ji

    ++

    +

    +++

    +

    +=

    +++

    ++++++

    ++

    22)(

    1

    )(

    21

    22))((4

    )2

    ()(

    2

    ,1,1,1,1

    2

    ,

    2

    ,1,,1

    ,

    ,1,11,1,1,11,11,11,1

    ,

    2,1,1

    2

    ,1,,1

    ,

    ,

    2

    xx

    p

    x

    p

    x

    v

    y

    u

    yx

    uv

    x

    u

    x

    uu

    tx

    u

    +

    +

    +

    +

    =

    22

    222

    2

    2211

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    Procedure

    The remaining derivatives are first spatial derivatives, namely, u/x,v/y,,/x,and /y,replaced by second-order central differences

    t

    v

    ytyv

    ty

    v

    ty

    v

    t

    u

    xtxu

    tx

    u

    tx

    u

    t

    +

    +

    +

    +

    +

    +

    +

    =

    2222

    2

    2

    x

    uu

    x

    u jijit

    ji

    +=

    +

    2

    ,1,1

    ,

    The other remaining derivatives are first time derivatives, /t, u/t,and v/t.

    /t has already been obtained from (6.9)

    u/t, and v/t can be obtained, analogous to the form of /t

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    Procedure

    We now have known values at time t for all three terms

    on the right side of the above equation.

    This allows the calculation of density at time t+t.

    Repeat the above procedures to find the remainingflow-field variables at grid point (i,j) at time t+t.

    +

    +

    +=+

    2

    )(2

    ,

    2

    2

    ,,,

    t

    ttt

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

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    The essence of the Lax-Wendroff methodObtain explicitly the flow-field variables at grid point (i,j) at time t+tfrom the known flow-field variables at grid points (i,j), (I+1,j), (I-1,j),

    and (i,j+1) at time t.

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    Discussion on the technique

    It has second order accuracy in both space and time.

    The idea is straightforward, but algebra is lengthy.

    Most of the lengthy algebra is associated with the second timederivative in Eqs. (6.6) to (6.8).

    +

    +

    +=+2

    )(2

    ,

    2

    2

    ,

    ,,

    t

    t

    vt

    t

    vvv

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    +

    +

    +=+

    2

    )( 2

    ,

    2

    2

    ,

    ,,

    t

    t

    et

    t

    eee

    t

    ji

    t

    ji

    t

    ji

    tt

    ji

    (6.7)

    (6.8)

    +

    +

    +=+2

    )(2

    ,

    2

    2

    ,

    ,,

    t

    t

    ut

    t

    uuu

    t

    ji

    t

    ji

    t

    ji

    tt

    ji (6.6)

    Much of this algebra can be cut by MacCormacks techniques