View question

The stagnation pressures at the inlet and exit of a subsonic intake are 100 kPa and 98 kPa, respectively. The pressure recovery of this intake will be ______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)

The stagnation pressures at the inlet and exit of a subsonic intake are 100 kPa and 98 kPa, respectively. The pressure recovery of this intake will be ______ (accurate to two decimal places). (GATE-Aerospace-Engineering-2018)


Asked On2019-04-10 14:03:38 by:naikaumprakash

Taged users:


Likes:
Be first to like this question

Dislikes:
Be first to dislike this question
  Like  Dislike

Comments


Type your comment here