When mach number is equal to one then the flow is ___________
A. Subsonic flow
B. Transonic flow
C. Supersonic flow
D. None of the mentioned
Answer:A
When mach number is equal to one then the flow is ___________
A. Subsonic flow B. Transonic flow C. Supersonic flow D. None of the mentioned
Explanation: For transonic flow mach number is equal to one.