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Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

Zienkiewicz O.C., Taylor R.L. Vol. 3. The finite - tiera.ru

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Equation of state<br />

p ˆ RT<br />

c p<br />

ˆ RT ˆ … ÿ 1† T …3:15†<br />

In the above equation R ˆ c p ÿ c v is used. <strong>The</strong> following forms of non-dimensional<br />

equations are useful to relate the speed of sound, temperature, pressure, energy, etc.<br />

E ˆ T ‡ 1<br />

2 u i u i<br />

c 2 ˆ… ÿ 1†T …3:16†<br />

p ˆ… ÿ 1† E ÿ 1 Ui Ui 2<br />

<strong>The</strong> above non-dimensional equations are convenient when coding the CBS<br />

algorithm. However, the dimensional form will be retained in this and other chapters<br />

for clarity.<br />

<strong>3.</strong>2 Characteristic-based split (CBS) algorithm<br />

<strong>3.</strong>2.1 <strong>The</strong> split ± general remarks<br />

<strong>The</strong> split follows the process initially introduced by Chorin 1;2 for incompressible ¯ow<br />

problems in the ®nite di€erence context. A similar extension of the split to ®nite<br />

element formulation for di€erent applications of incompressible ¯ows have been<br />

carried out by many authors. 3ÿ27 However, in this chapter we extend the split to<br />

solve the ¯uid dynamics equations of both compressible and incompressible forms<br />

using the characteristic±Galerkin procedure. 28ÿ46 <strong>The</strong> algorithm in its full form<br />

was ®rst introduced in 1995 by <strong>Zienkiewicz</strong> and Codina 28;29 and followed several<br />

years of preliminary research. 47ÿ51<br />

Although the original Chorin split 1;2 could never be used in a fully explicit code, the<br />

new form is applicable for fully compressible ¯ows in both explicit and semi-implicit<br />

forms. <strong>The</strong> split provides a fully explicit algorithm even in the incompressible case for<br />

steady-state problems now using an `arti®cial' compressibility which does not a€ect<br />

the steady-state solution. When real compressibility exists, such as in gas ¯ows, the<br />

computational advantages of the explicit form compare well with other currently<br />

used schemes and the additional cost due to splitting the operator is insigni®cant.<br />

Generally for an identical cost, results are considerably improved throughout a<br />

large range of aerodynamical problems. However, a further advantage is that both<br />

subsonic and supersonic problems can be solved by the same code.<br />

<strong>3.</strong>2.2 <strong>The</strong> split ± temporal discretization<br />

Characteristic-based split (CBS) algorithm 67<br />

We can discretize Eq. (<strong>3.</strong>4) in time using the characteristic±Galerkin process. Except<br />

for the pressure term this equation is similar to the convection±di€usion equation

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