Shock effect in a nozzle is felt in
A. divergent portion
B. straight portion
C. convergent portion
D. throat
Answer:A
Shock effect in a nozzle is felt in
A. divergent portion B. straight portion C. convergent portion D. throat
Explanation: Shock effect in a nozzle is felt in divergent portion. For a nozzle to have a supersonic outlet, the speed at the throat should be definitely sonic and the nozzle should be divergent from the throat section.