Question

A supersonic flow in a constant area duct at Mach number M, encounter tamp of
angle 8, (see Figure 1). The resulting oblique shock angle is then reflected from the
top wall. For the reflected shock, the turn angle is e, and the shock angle is B,
I
Figure!
Use the weak shock solution from the -B M plot shown in Figure 2 to choose the
correct option from the following
(A)
BB
(B) B. <B​

Answer 1

In mathematics, the irrational numbers are all the real numbers which are not rational numbers. That is, irrational numbers cannot be expressed as the ratio of two integers. ... For example, the decimal representation of π starts with 3.14159, but no finite number of digits can represent π exactly, nor does it repeat.