Column I | Column II |
A. Thrust | (p) F/A |
B. Pressure | (q) Force |
C. Atmospheric pressure | (r) Decrease with altitude |
D. liquid pressure | (s) Monometer |
A) \[A\to (q);B\to (p);C\to (r);D\to (s)\]
B) \[A\to (r);B\to (p);C\to (q);D\to (s)\]
C) \[A\to (p);B\to (r);C\to (s);D\to (q)\]
D) \[A\to (s);B\to (q);C\to (p);D\to (r)\]
Correct Answer: A
Solution :
\[A\to (q);B\to (p);C\to (r);D\to (s)\]You need to login to perform this action.
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