Discussion
Total pressure recovery of an inlet is defined as the ratio of
Answer: C
It is the single figure that expresses how much of the available energy the intake has preserved. A loss of one per cent in recovery typically costs more than one per cent in thrust, which is why intake design receives such attention on high speed aircraft.
No comment is present. Be the first to comment.
Loading…
Post your comment
Please log in or register to post a comment.
Examination Categories
- SSC Exams
- Banking Exams
- Teaching Exams
- Civil Services Exams
- Railways Exams
- Engineering Recruitment Exams
- Defence Exams
- State Government Exams
- Police Exams
- Insurance Exams
- Nursing Exams
- Other Government Exams
- NRA CET
- PG Entrance Exams
- Campus Placement
- MBA Entrance Exams
- CUET and UG Entrance
- Judiciary Exams
- Regulatory Body Exams
- Software Development