Attached weak oblique shocks over the same wedge are sketched for three different upstream Mach numbers \(M_1, M_2, M_3 > 1\). Which ordering is TRUE?

Step 1: Dependence of shock angle on Mach number for fixed wedge angle (weak branch).
For a given wedge deflection \(\theta\) and weak attached shock, the shock angle \(\beta\) satisfies the \(\theta\)–\(\beta\)–\(M\) relation. As the upstream Mach number \(M\) increases, the weak-shock angle \(\beta\) decreases, approaching the Mach angle \(\mu=\sin^{-1}(1/M)\).
Conversely, as \(M\) approaches \(1^+\), \(\beta\) increases toward \(90^\circ\) (normal shock limit).
Step 2: Read the sketches qualitatively.
From left to right, the drawings show shocks that are (i) at a moderate angle to the wedge, (ii) tightly hugging the wedge (small \(\beta\)), and (iii) very open/near-normal (large \(\beta\)).
Thus the corresponding Mach numbers satisfy \[ \text{smallest }\beta \Rightarrow \text{largest }M, \qquad \text{largest }\beta \Rightarrow \text{smallest }M. \] Therefore, \[ M_2\; \text{(middle)}\; >\; M_1\; \text{(left)}\; > \; M_3\; \text{(right)}. \] \[ \boxed{M_3 < M_1 < M_2} \]
The lift per unit span for a spinning circular cylinder in a potential flow is 6 N/m. The free-stream velocity is 30 m/s, and the density of air is 1.225 kg/m\(^3\). The circulation around the cylinder is __________ m\(^2\)/s (rounded off to two decimal places).
In a centrifugal compressor, the eye tip diameter is 10 cm. For a shaft rotational speed of 490 rotations per second, the tangential speed at the inducer tip is _________ m/s (rounded off to one decimal place).
An aircraft is flying at an altitude of 4500 m above sea level, where the ambient pressure, temperature, and density are 57 kPa, 259 K, and 0.777 kg/m\(^3\), respectively. The speed of the aircraft \( V \) is 230 m/s. Gas constant \( R = 287 \, {J/kg/K} \), and specific heat ratio \( \gamma = 1.4 \). If the stagnation pressure is \( p_0 \), and static pressure is \( p \), the value of \[ \frac{p_0 - p}{\frac{1}{2} \rho V^2} \] is __________ (rounded off to two decimal places).
A supersonic stream of an ideal gas at Mach number \( M_1 = 5 \) is turned by a ramp, as shown in the figure. The ramp angle is 20°. The pressure ratio is \( \frac{p_2}{p_1} = 7.125 \) and the specific heat ratio is \( \gamma = 1.4 \). The pressure coefficient on the ramp surface is ___________ (rounded off to two decimal places).
Air at Mach number \(M=2\) expands around a convex corner to \(M=3\). What is the angle \(\delta\) between the forward and rearward Mach lines of the Prandtl–Meyer expansion fan (in degrees)? Given \(\nu(3)=49.76^\circ\) and \(\nu(2)=26.38^\circ\).

Courage : Bravery :: Yearning :
Select the most appropriate option to complete the analogy.
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Select the most appropriate option to complete the above sentence.
A 4 × 4 digital image has pixel intensities (U) as shown in the figure. The number of pixels with \( U \leq 4 \) is:

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Select the most appropriate option to complete the above sentence.