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

–C p
–C p
–C p
1.5
1.0
0.5
0
–0.5
–1.0
1.5
1.0
0.5
0
–0.5
–1.0
1.5
1.0
0.5
0
–0.5
–1.0
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
X/C
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
X/C
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
X/C
Boundary layer±inviscid Euler solution coupling 211
–C p
–C p
–C p
coupling is not directly applicable in problems where boundary layer separation
occurs, many studies are available to deal with separated ¯ows. 94ÿ96 We do not
give any further details of viscous±inviscid coupling here and the reader can refer
to the quoted references and Appendix E.
(c)
1.5
1.0
0.5
0
–0.5
–1.0
1.5
1.0
0.5
0
–0.5
–1.0
1.5
1.0
0.5
0
–0.5
–1.0
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
X/C
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
X/C
0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0
X/C
Fig. 6.28 (Continued) (c) coef®cient of pressure distribution at 20%, 44%, 65%, 80%, 90% and 95% of
wing span, line±numerical 34 and circle±experimental. 83