Research Article
Micropolar Couple Stress Nanofluid Flow by Non-Fourier’s-Law Heat Flux Model past a Stretching Sheet
Table 6
Numerical values of local skin friction coefficient
, local wall couple stress
, local Nusselt number
, and local Sherwood number
.
| | | | | | | | | | | | | | | | | |
| 0.72 | 0.2 | 0.2 | 0.3 | 0.5 | 0.3 | 0.3 | 0.4 | 0.9 | 1 | 0.2 | 0.1 | 0.2 | 0.87083 | 0.36505 | 0.35420 | 0.77366 | 1.00 | — | — | — | — | — | — | — | — | — | — | — | — | 0.87975 | 0.40984 | 0.40984 | 0.78631 | 1.20 | — | — | — | — | — | — | — | — | — | — | — | — | 0.88446 | 0.36802 | 0.44153 | 0.79387 | 0.72 | 0.5 | — | — | — | — | — | — | — | — | — | — | — | 0.70965 | 0.28433 | 0.39561 | 0.80501 | — | 1.0 | — | — | — | — | — | — | — | — | — | — | — | 0.46798 | 0.15266 | 0.44175 | 0.84252 | — | 0.2 | 0.5 | — | — | — | — | — | — | — | — | — | — | 0.87083 | 0.36505 | 0.35420 | 0.77366 | — | — | 1.0 | — | — | — | — | — | — | — | — | — | — | 0.87083 | 0.36505 | 0.35420 | 0.77366 | — | — | 0.2 | 0.5 | — | — | — | — | — | — | — | — | — | 0.87326 | 0.36540 | 0.36315 | 0.77436 | — | — | — | 1.0 | — | — | — | — | — | — | — | — | — | 0.83617 | 0.32736 | 0.45194 | 0.68164 | — | — | — | 0.3 | 1.0 | — | — | — | — | — | — | — | — | 1.02372 | 0.44399 | 0.31913 | 0.74550 | — | — | — | — | 1.5 | — | — | — | — | — | — | — | — | 1.08394 | 0.44947 | 0.33095 | 0.65811 | — | — | — | — | 0.5 | 0.6 | — | — | — | — | — | — | — | 0.86399 | 0.36376 | 0.40495 | 0.76530 | — | — | — | — | — | 0.9 | — | — | — | — | — | — | — | 0.85877 | 0.36285 | 0.45056 | 0.75959 | — | — | — | — | — | 0.3 | 0.6 | — | — | — | — | — | — | 0.87075 | 0.36498 | 0.34987 | 0.79075 | — | — | — | — | — | — | 0.9 | — | — | — | — | — | — | 0.87068 | 0.36491 | 0.34575 | 0.80706 | — | — | — | — | — | — | 0.3 | 0.8 | — | — | — | — | — | 0.86065 | 0.36190 | 0.22236 | 0.72602 | — | — | — | — | — | — | — | 1.2 | — | — | — | — | — | 0.85112 | 0.35902 | 0.10804 | 0.68622 | — | — | — | — | — | — | — | 0.4 | 1.2 | — | — | — | — | 0.87074 | 0.36489 | 0.32551 | 0.88681 | — | — | — | — | — | — | — | — | 1.5 | — | — | — | — | 0.87066 | 0.36476 | 0.30043 | 0.98566 | — | — | — | — | — | — | — | — | 0.9 | 1.5 | — | — | — | 0.81175 | 0.31635 | 0.35527 | 0.82618 | — | — | — | — | — | — | — | — | — | 2.0 | — | — | — | 0.76402 | 0.27927 | 0.36653 | 0.83395 | — | — | — | — | — | — | — | — | — | 1.0 | 0.5 | — | — | 0.87077 | 0.36495 | 0.32069 | 0.90032 | — | — | — | — | — | — | — | — | — | — | 0.8 | — | — | 0.87070 | 0.36486 | 0.29019 | 1.01546 | — | — | — | — | — | — | — | — | — | — | — | 0.2 | — | 0.86991 | 0.36468 | 0.32836 | 0.83265 | — | — | — | — | — | — | — | — | — | — | — | 0.3 | — | 0.86901 | 0.36436 | 0.31559 | 0.84398 | — | — | — | — | — | — | — | — | — | — | — | 0.2 | 0.3 | 0.87012 | 0.36480 | 0.33036 | 0.80542 | — | — | — | — | — | — | — | — | — | — | — | — | 0.4 | 0.86942 | 0.36457 | 0.31742 | 0.79865 |
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