Given the velocity vector V = ax i + by I, where a, b = constant. Plot the streamlines of flow and explain whether stagnation point occurs.

Streamline Analysis and Stagnation Point

Problem Statement

Given the velocity vector V = ax i + by j, where a and b are constants:

  1. Plot the streamlines of flow
  2. Explain whether stagnation point occurs

1. Apply Continuity Equation

Given velocity components:
u = ax
v = by

For an incompressible flow, the continuity equation must be satisfied:
∂u/∂x + ∂v/∂y = 0

Step 1.1: Calculate the partial derivatives
∂u/∂x = a
∂v/∂y = b

Step 1.2: Apply the continuity equation
a + b = 0
Therefore, b = -a

Step 1.3: Update the velocity components
u = ax
v = -ay

The velocity field is now: V = ax i – ay j

2. Find Streamline Equations

Streamlines are curves whose tangent at any point is in the direction of the velocity vector at that point.

Step 2.1: Write the streamline differential equation
dx/u = dy/v
dx/ax = dy/(-ay)

Step 2.2: Separate variables and integrate
(dx/x) = -(dy/y)
∫(dx/x) = -∫(dy/y)
ln|x| = -ln|y| + C₁
ln|x| + ln|y| = C₁
ln|xy| = C₁

Step 2.3: Simplify to get the equation of streamlines
|xy| = e^(C₁) = C
Therefore, xy = C (where C is a constant)

The streamlines are represented by the equation: xy = C

3. Analyze Streamline Behavior

The equation xy = C represents a family of hyperbolas with the x and y axes as asymptotes.

Let’s analyze special cases:

Case 1: When C = 0
xy = 0
This implies either x = 0 or y = 0
So the x and y axes themselves are streamlines.

Case 2: When C > 0 (e.g., C = 1)
xy = 1 or y = 1/x
For positive x, y is also positive
For negative x, y is also negative
So these streamlines lie in the first and third quadrants.

Case 3: When C < 0 (e.g., C = -1)
xy = -1 or y = -1/x
For positive x, y is negative
For negative x, y is positive
So these streamlines lie in the second and fourth quadrants.

x y (0,0) Quadrant I Quadrant II Quadrant III Quadrant IV C = 0 C > 0 C < 0 Stagnation point
The streamlines form a family of hyperbolas with different values of C.

4. Identify Stagnation Point

A stagnation point is a point in the flow where the velocity becomes zero.

Step 4.1: Set both velocity components to zero
u = ax = 0
v = -ay = 0

Step 4.2: Solve for coordinates
For u = 0: x = 0 (since a ≠ 0)
For v = 0: y = 0 (since a ≠ 0)

Therefore, the stagnation point occurs at the origin (0, 0).

The stagnation point exists at the origin (0, 0)

5. Determine Flow Direction

Assuming a > 0, let’s analyze the flow direction in each quadrant:

First Quadrant (x > 0, y > 0):
u = ax > 0 (flow to the right)
v = -ay < 0 (flow downward)
Net flow: downward to the right

Second Quadrant (x < 0, y > 0):
u = ax < 0 (flow to the left)
v = -ay < 0 (flow downward)
Net flow: downward to the left

Third Quadrant (x < 0, y < 0):
u = ax < 0 (flow to the left)
v = -ay > 0 (flow upward)
Net flow: upward to the left

Fourth Quadrant (x > 0, y < 0):
u = ax > 0 (flow to the right)
v = -ay > 0 (flow upward)
Net flow: upward to the right

At the stagnation point, streamlines from different directions intersect.

Conclusion

We have analyzed the flow field with velocity vector V = ax i + by j with a + b = 0:

1. The streamlines are described by the equation xy = C, which represents a family of hyperbolas with different values of C.

2. Special streamlines include:
– The x and y axes (when C = 0)
– Hyperbolas in the first and third quadrants (when C > 0)
– Hyperbolas in the second and fourth quadrants (when C < 0)

3. A stagnation point exists at the origin (0, 0), where both velocity components are zero.

4. At the stagnation point, streamlines from different directions intersect, which is a characteristic feature of stagnation points in fluid flows.

Physical Interpretation

This flow field, known as a hyperbolic flow, has several important characteristics:

  • The flow exhibits a stagnation point at the origin where fluid particles come to rest
  • The streamlines form orthogonal hyperbolas, with the coordinate axes as asymptotes
  • This flow pattern is similar to what we observe when a fluid approaches a flat plate perpendicular to the flow direction
  • Near the stagnation point, fluid elements are stretched in one direction and compressed in the perpendicular direction
  • This type of flow is important in many practical applications, such as the flow around the leading edge of an airfoil or blunt body
  • At the stagnation point, the maximum pressure in the flow field occurs (according to Bernoulli’s equation)
  • The flow pattern shows how fluid elements deform as they approach and move away from the stagnation point

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