Numerical and Analytical Investigation for Darcy-Forchheimer Flow of a Williamson Fluid over a Riga Plate with Double Stratification and Cattaneo-Christov Dual Flux

Table 2

Numerical and analytical computation of local skin friction coefficient, local Nusselt number, and local Sherwood number for various values of , and .

We					Skin friction coefficient		Local Nusselt number		Local Sherwood number
					Numerical	Analytical	Numerical	Analytical	Numerical	Analytical
0.0	0.2	0.4	0.3	0.3	-1.21627	-1.21624	2.06338	2.06344	1.46840	1.46841
0.1					-1.19072	-1.19070	2.05471	2.05477	1.46383	1.46385
0.2					-1.16263	-1.16259	2.04481	2.04487	1.45858	1.45860
0.3					-1.13089	-1.13083	2.03314	2.03319	1.45233	1.45235
0.4					-1.09319	-1.09164	2.01848	2.01859	1.44438	1.44442
0.5					-0.99995	-0.99998	1.99720	1.99782	1.43257	1.43294
0.2	0.0	0.4	0.3	0.3	-1.07827	-1.07818	2.07408	2.07422	1.47298	1.47303
	0.1				-1.12135	-1.12130	2.05904	2.05913	1.46558	1.46561
	0.2				-1.16263	-1.16259	2.04481	2.04487	1.45858	1.45860
	0.3				-1.20228	-1.20225	2.03132	2.03136	1.45194	1.45195
	0.4				-1.24046	-1.24042	2.01851	2.01853	1.44563	1.44564
	0.5				-1.27728	-1.27725	2.00630	2.00634	1.43961	1.43964
0.2	0.2	0.0	0.3	0.3	-1.05656	-1.05652	2.06805	2.06811	1.47074	1.47076
		0.3			-1.13706	-1.13702	2.05038	2.05043	1.46149	1.46151
		0.5			-1.18763	-1.18758	2.03940	2.03945	1.45575	1.45576
		0.8			-1.25946	-1.25942	2.02397	2.02406	1.44768	1.44773
		1.0			-1.30495	-1.30544	2.01430	2.01498	1.44262	1.44322
0.2	0.2	0.4	-1.0	0.3	-0.68939	-0.68936	1.22935	1.22940	0.91349	0.91350
			-0.5		-0.83580	-0.83579	1.47333	1.47339	1.07673	1.07675
			0.0		-1.02546	-1.02543	1.79633	1.79639	1.29221	1.29223
			0.5		-1.26411	-1.26408	2.24148	2.24153	1.59103	1.59105
			1.0		-1.55195	-1.55182	2.88826	2.88923	2.03343	2.03242
0.2	0.2	0.4	0.3	0.0	-1.29871	-1.29869	1.99254	1.99255	1.43332	1.43333
				0.5	-1.07378	-1.07374	2.07612	2.07619	1.47399	1.47401
				1.0	-0.85646	-0.85641	2.14556	2.14568	1.50882	1.50886
				1.5	-0.64420	-0.64411	2.20587	2.20586	1.53970	1.53989
				2.0	-0.43568	-0.43431	2.25965	2.26084	1.56771	1.57081