The relationship between traffic flow rate (q) and density (D) is shown in the figure
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The shock wave condition is depicted by
(A) flow with respect to point $1\left(q_{1}=q_{\max }\right)$
(B) flow changing from point 2 to point $6\left(\mathrm{q}_{2}>\mathrm{q}_{6}\right)$
(C) flow changing from point 3 to point $7\left(\mathrm{q}_{3}<\mathrm{q} 7\right)$
(D) flow with respect to point 4 and point $5\left(\mathrm{q}_{4}=\mathrm{q} 5\right)$
The shock wave condition is depicted by
(A) flow with respect to point $1\left(q_{1}=q_{\max }\right)$
(B) flow changing from point 2 to point $6\left(\mathrm{q}_{2}>\mathrm{q}_{6}\right)$
(C) flow changing from point 3 to point $7\left(\mathrm{q}_{3}<\mathrm{q} 7\right)$
(D) flow with respect to point 4 and point $5\left(\mathrm{q}_{4}=\mathrm{q} 5\right)$
Question ID - 1 | SaraNextGen Top Answer The relationship between traffic flow rate (q) and density (D) is shown in the figure
The shock wave condition is depicted by
(A) flow with respect to point $1\left(q_{1}=q_{\max }\right)$
(B) flow changing from point 2 to point $6\left(\mathrm{q}_{2}>\mathrm{q}_{6}\right)$
(C) flow changing from point 3 to point $7\left(\mathrm{q}_{3}<\mathrm{q} 7\right)$
(D) flow with respect to point 4 and point $5\left(\mathrm{q}_{4}=\mathrm{q} 5\right)$
The relationship between traffic flow rate (q) and density (D) is shown in the figure
The shock wave condition is depicted by
(A) flow with respect to point $1\left(q_{1}=q_{\max }\right)$
(B) flow changing from point 2 to point $6\left(\mathrm{q}_{2}>\mathrm{q}_{6}\right)$
(C) flow changing from point 3 to point $7\left(\mathrm{q}_{3}<\mathrm{q} 7\right)$
(D) flow with respect to point 4 and point $5\left(\mathrm{q}_{4}=\mathrm{q} 5\right)$
flow changing from point 2 to point $6\left(\mathrm{q}_{2}>\mathrm{q}_{6}\right)$