Table 1.

Numerical results of the skin friction (wall drag) and Nusselt number (heat flux). The default values are: $\lambda =2/10$, $M=2/10$, $Fr=1$, $\gamma =2/10$, $K=2/10$, $Le=1$, $Nb=2/10$, $Nt=1/10$, $Pr=1$, $Rd=2/10$.

$\mathit{\lambda }$	$\mathit{Fr}$	$\mathit{\gamma }$	K	$\mathit{Le}$	M	$\mathit{Nb}$	$\mathit{Nt}$	$\mathit{Pr}$	$\mathit{Rd}$	$-{\mathit{Re}}_{\mathit{x}}^{1/2}{\mathit{C}}_{\mathit{fx}}$	$-{\mathit{Re}}_{\mathit{x}}^{-1/2}{\mathit{Nu}}_{\mathit{x}}$	$-{\mathit{Re}}_{\mathit{x}}^{-1/2}{\mathit{Sh}}_{\mathit{x}}$
$0.0$										$1.1199$	$0.4129$	$0.5306$
$0.3$										$1.2456$	$0.3962$	$0.5175$
$0.6$										$1.3601$	$0.3822$	$0.5067$
	$0.0$									$1.1786$	$0.5115$	$0.4085$
	$0.3$									$1.3065$	$0.4027$	$0.3957$
	$0.6$									$1.4242$	$0.3981$	$0.3933$
		$0.0$								$1.3514$	$0.4172$	$0.5341$
		$0.3$								$1.4492$	$0.3941$	$0.5159$
		$0.6$								$1.5233$	$0.3744$	$0.5007$
			$0.0$							$1.4235$	$0.4050$	$0.4003$
			$0.3$							$1.4235$	$0.3969$	$0.7075$
			$0.6$							$1.4235$	$0.3931$	$0.9137$
				$0.4$						$--$	$0.4097$	$0.3353$
				$0.8$						$--$	$0.4040$	$0.4581$
				$1.2$						$--$	$0.3991$	$0.5846$
					$0.0$					$1.4089$	$0.4039$	$0.5236$
					$0.3$					$1.4429$	$0.3984$	$0.5193$
					$0.6$					$1.5983$	$0.3838$	$0.5079$
						$0.4$				$--$	$0.3650$	$0.5840$
						$0.8$				$--$	$0.2999$	$0.6142$
						$1.2$				$--$	$0.2445$	$0.6236$
							$0.0$			$--$	$0.4123$	$0.6312$
							$0.3$			$--$	$0.3807$	$0.3263$
							$0.6$			$--$	$0.3520$	$0.0868$
								$0.6$		$--$	$0.3071$	$0.4292$
								$1.2$		$--$	$0.4445$	$0.5693$
								$2.0$		$--$	$0.5784$	$0.7616$
									$0.0$	$--$	$0.4649$	$0.4990$
									$0.5$	$--$	$0.3369$	$0.5445$
									$1.0$	$--$	$0.1025$	$0.8359$