Figure 6:
The pressure rise verses flow rate when
𝛼
=
0
.
0
1
,
𝑏
=
0
.
6
,
𝑑
=
0
.
8
,
𝜀
=
0
.
3
,
𝜆
1
=
0
.
4
,
D
a
=
0
.
5
, and
𝜙
=
𝜋
/
4
.
