where is the numerical approximation to for various values of.
Figure 3 Velocity profile f ′ for various values of ϕ.
Numerical results are given for various values of the parameters.
D as a function of RE, parametrized with respect to ρsz (for various values of c) (a) and c (for various values of ρsz) (b).
Figure 5 Velocity, temperature, and concentration profiles for various values of Lewis number (Le). Figure 6 Velocity, temperature, and concentration profiles for various values of velocity exponent (m).
D as a function of RE, parametrized with respect to (a) ρsz (for various values of g) and (b) g (for various values of ρ s z).
The results are given for various values of the external pressure and different shell aspect ratios.
The theoretical model's stability is determined with various values of design parameters at the steady state.
These optimal positions are reported for various values of plate aspect ratios and cutout sizes.
Numerical simulations have been carried out for various values of Prandtl (Pr) and Rayleigh (Ra) numbers.
By solving the model for various values of ε, the approximated Pareto frontier is constructed.
