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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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186 Compressible high-speed gas ¯ow<br />

G p<br />

1.80<br />

1.60<br />

1.40<br />

1.20<br />

1.00<br />

0.80<br />

0.60<br />

0.40<br />

0.20<br />

0<br />

–0.20<br />

–<strong>3.</strong>00 –2.00 –1.00 0 1.00 2.00 <strong>3.</strong>00<br />

(a)<br />

X<br />

Mach number<br />

(b)<br />

4.00<br />

<strong>3.</strong>00<br />

2.00<br />

1.00<br />

MUSCL<br />

CBS: Anisotropic Shock Capture<br />

CBS: Second Derivative Shock Capture<br />

0<br />

–<strong>3.</strong>00 –2.00 –1.00 0 1.00 2.00 <strong>3.</strong>00<br />

X<br />

Fig. 6.10 Supersonic ¯ow past a full cylinder. 56 M ˆ 3, comparison of (a) coef®cient of pressure, (b) Mach<br />

number distribution along the mid-height and cylinder surface.

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