Effects of Slip Factors and Couple Stresses for Stagnation Point Flow over a Moving Plate

Figure 2

The ħ curves for 6th order of approximation of HAM when 𝜆=0.2, 𝜉=1. (a) for 𝑓^′′(0), (b) for 𝑔^′(0), (c) for ℎ^′(0).

(a)

(b)

(c)