Discussion
A flow at Mach 1 is turned through 130.45 degrees round a convex corner. At the end of the turn
Answer: B
That angle is the maximum value of the Prandtl-Meyer function for air, reached as the Mach number grows without bound and the static pressure tends to zero. The stagnation pressure is untouched throughout, since the process remains isentropic; it is the static pressure that vanishes.
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