Concept:
The Mach number (M) is defined as the ratio of local flow velocity to the local speed of sound. Flow regimes are classified based on this number.
Step 1: Categorize the Mach regimes.
• D. Subsonic: $M < 0.8$
• B. Transonic: $0.8 \le M \le 1.2$
• A. Supersonic: $1.2 < M < 5.0$
• C. Hypersonic: $M \ge 5.0$
Step 2: Escalating order.
Arranging from the smallest to largest Mach number gives: Subsonic $\rightarrow$ Transonic $\rightarrow$ Supersonic $\rightarrow$ Hypersonic (D, B, A, C).