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Question

Pressure drag as per boundary layer theory is function of

The correct answer is
shape of body and separation of flow

Pressure drag is a significant component of the total drag experienced by an object moving through a fluid. Boundary layer theory provides insights into how this type of drag arises.

Understanding Pressure Drag Components

Pressure drag, also known as form drag, is primarily caused by the pressure difference between the front and the rear surfaces of a body. This pressure difference is a direct consequence of the fluid flow pattern around the body.

Boundary Layer Theory and Pressure Drag

According to boundary layer theory, the interaction between the fluid and the body's surface is crucial. The theory explains:

  • Body Shape: The contour and geometry of the body significantly influence how the fluid flows around it. A streamlined shape generally maintains attached flow, leading to lower pressure drag. Conversely, a blunt shape can cause flow separation.
  • Flow Separation: This occurs when the boundary layer detaches from the surface of the body. Separation typically happens in regions of adverse pressure gradient (pressure increasing in the direction of flow), often near the rear of the body. This separation creates a turbulent wake region behind the body where the pressure is significantly lower than the pressure on the front surface, resulting in substantial pressure drag.

Why Other Options Are Less Complete

  • Shape of body: While crucial, shape alone doesn't fully capture the mechanism without considering how the flow *behaves* around that shape, specifically separation.
  • Dimensions of body: Body dimensions influence the overall magnitude of drag but are not the primary *functional* determinants explained by boundary layer theory regarding the *nature* of pressure drag.
  • Flow direction: The effect of flow direction is implicitly considered within the body's shape and the resulting flow patterns, including separation.

Conclusion

Therefore, pressure drag, as understood through boundary layer theory, is fundamentally a function of the shape of the body and the occurrence of flow separation around it.

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Important Questions from Boundary Layer Theory

  1. Friction drag is generally larger than the pressure drag in _______.

  2. When a fluid flows along a solid boundary, more and more fluid gets retarded in the vicinity of the boundary. This deceleration is accompanied by:

  3. A plate of 500 mm × 200 mm has been placed longitudinally in a stream of an oil which flows with a velocity of 1.0 m/s. The kinematic viscosity of the oil was 0.5 stoke. The thickness of the boundary layer at the trailing edge is _______.

  4. As defined by Prandtl, in convective heat transfer, a thin layer next to the wall where shear stress is confined is called _____.

  5. Thickness of laminar boundary layer on flat plate:

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