Aerospace Engineering > GATE 2024 >
In the context of steady, inviscid, incompressible flows, consider the superposition of a uniform flow with speed U along the positive x-axis (from left to right), and a source of strength A located at the origin. Which one of the following statements is NOT true regarding the location of the stagnation point of the resulting flow?
A
It is located to the left of the origin
B
It moves closer to the origin for increasing A, while U is held constant
C
It moves closer to the origin for increasing U, while A is held constant
D
It is located along the x-axis

Correct : c

Similar Questions

On Day 1, an aircraft flies with a speed of V1 m/s at an altitude where the temperature is T1 K. On Day 2, the same aircraft flies with a speed of √1.2 * V1 m/s...
#30 MCQ
Consider a steady, isentropic, supersonic flow (Mach number M > 1) entering a Convergent-Divergent (CD) duct as shown in the figure. Which one of the followi...
#31 MCQ
Consider steady, incompressible, inviscid flow past two airfoils shown in the figure. The coefficient of pressure at the trailing edge of the airfoil with finit...
#32 MCQ

Related Topics

No tags found

Unique Visitor Count

Total Unique Visitors

Loading......