Top

Discussion

Which of the following statement is correct relating to rocket engines ?

  • A.The combustion chamber in a rocket engine is directly analogous to the reservoir of a super sonic wind tunnel
  • B.all of the above
  • C.The stagnation conditions exist at the combustion chamber
  • D.The exit velocities of exhaust gases are much higher than those in jet engine

Answer: B

No answer description available for this question.
 

No comment is present. Be the first to comment.
Loading…

Post your comment

Subject Categories

Examination Categories

About Us

ReadySetScores

Copyright © 2025 ReadySetScores . All Rights Reserved . With