1 / 13

Pressure, Drag and Lift for Uniform Flow Over a Cylinder

Pressure, Drag and Lift for Uniform Flow Over a Cylinder. a 2 = 1. Pressure, Drag and Lift for Uniform Flow Over a Cylinder. Along the cylinder, r = a , the velocity components become:. u θ is maximum at θ = π /2 and 3 π /2; zero at θ = 0 and θ = π.

Télécharger la présentation

Pressure, Drag and Lift for Uniform Flow Over a Cylinder

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Pressure, Drag and Lift for Uniform Flow Over a Cylinder a2 = 1

  2. Pressure, Drag and Lift for Uniform Flow Over a Cylinder Along the cylinder, r = a, the velocity components become: uθ is maximum at θ = π/2 and 3 π /2; zero at θ = 0 and θ = π

  3. The pressure distribution can be obtained using Bernoulli’s equation: dimensionless pressure coefficient Cp

  4. The drag on the cylinder may be calculated through integration of the pressure over the cylinder surface: Fy Fx The drag on the cylinder acts parallel to the flow. The lift is perpendicular to the flow:

  5. Pressure, Drag and Lift for Uniform Flow Over a Rotating Cylinder Along the cylinder, r = a, the velocity components become:

  6. The pressure distribution can be obtained using Bernoulli’s equation: dimensionless pressure coefficient Cp

  7. The drag and lift can be obtained by integrating the pressure over the cylinder surface pc : Still no drag for a rotating cylinder There is lift proportional to density, upstream velocity, and strength of vortex -- Kutta – Jukowski law Lifting effect for rotating bodies in a free stream is called Magnus effect

  8. Example of Pressure, Drag and Lift for Uniform Flow Over a Cylinder 3 m The drag on the cylinder may be calculated through integration of the pressure over half the cylinder surface, from 0 to π. u = 20 m/s That’ll be with the outside pressure, inside pressure p0 should also be considered:

  9. 3 m u = 20 m/s

  10. The lift on the object may be calculated through integration of the pressure over half the cylinder surface, from 0 to π. 3 m u = 20 m/s

  11. 3 m u = 20 m/s

  12. Lift for half-cylinder, 3 m high, influenced by wind (air density) Gale Force tropical depres-sion tropical storm hurricane

  13. Lift for half-cylinder, 1 m high, influenced by flow (water density)

More Related