HTLS150/150C Computer Controlled Closed Hydrodynamic Tunnel for Low Speed, 150X150 mm

8.5.- 유압 채널
COMPUTER CONTROLLED CLOSED HYDRODYNAMIC TUNNEL FOR LOW SPEED, 150X150 MM - HTLS150/150C

혁신적인 시스템

The Computer Controlled Closed Hydrodynamic Tunnel for Low Speed, 150 x 150 mm, "HTHS150/150C", allows to test the hydrodynamics of bodies designed to work submerged in water and, with a correct design of the experiment, to study the aerodynamics of objects flying in air.

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일반적인 설명

The Computer Controlled Low Speed Hydrodynamic Tunnel, 150 x 150 mm, "HTLS150/150C", is a hydrodynamic tunnel in a closed water circuit flowing in the vertical plane. The water is circulated by a computer controlled variable speed pump. Different models and accessories are available, allowing a complete study of the hydrodynamics.

The unit includes several sections to reduce flow interference.

The working area consists of a constant section section, where the models are mounted for testing. It is manufactured with fused silica (quartz) windows on the front, back and top face for optical testing. This section includes a Pitot tube in its upper part to study static pressure, dynamic pressure and total pressure. It also includes a removable screen at the inlet to increase the turbulence of the flow.

This Computer Controlled Unit is supplied with the EDIBON Computer Control System (SCADA), and includes: The unit itself + a Control Interface Box + a Data Acquisition Board + Computer Control, Data Acquisition and Data Management Software Packages, for controlling the process and all parameters involved in the process.

연습 및 가이드

매뉴얼에 포함 된 가이드 실기 연습

  1. Extensive study of hydrodynamics and water flow studies.
  2. Study of flow visualization.
  3. Study of static pressure, dynamic pressure and total pressure using a Pitot tube.
  4. Study of the measurement of velocity using a Pitot tube.
  5. Study of turbulent and laminar flow.
  6. Study of cavitation in different models.
  7. Calibration of sensors.

장비로 수행 할 수있는 더 많은 실용적 연습

Additional practical possibilities to be carried out with the recommended additional elements (Not included):

  1. Visualization of flows around different resistor bodies:
  • Sphere Drag Model (HTLS7/150) (requires element HTLS150/150C-TARC).
  • Hemisphere Drag Model (HTLS8/150) (requires element HTLS150/150C-TARC).
  • Circular Plate Drag Model (HTLS9/150) (requires element HTLS150/150C-TARC).
  • Ring Drag Model (HTLS10/150) (requires element HTLS150/150C-TARC).
  • Square Plate Drag Model (HTLS11/150) (requires element HTLS150/150C-TARC).
  • Cylinder Drag Model (HTLS12/150) (requires element HTLS150/150C-TARC).
  • Paraboloid Drag Model (HTLS13/150) (requires element HTLS150/150C-TARC).
  • Dimpled Sphere Drag Model (HTLS14/150) (requires element HTLS150/150C-TARC).
  • Wing Drag Model (HTLS15/150) (requires element HTLS150/150C-TARC).
  • Airplane Drag Model (HTLS16/150) (requires element HTLS150/150C-TARC).
  1. Determination of the hydrodynamic drag coefficient and lift coefficient in different models:
  • Sphere Drag Model (HTLS7/150) (requires element HTLS150/150C-TARC).
  • Hemisphere Drag Model (HTLS8/150) (requires element HTLS150/150C-TARC).
  • Circular Plate Drag Model (HTLS9/150) (requires element HTLS150/150C-TARC).
  • Ring Drag Model (HTLS10/150) (requires element HTLS150/150C-TARC).
  • Square Plate Drag Model (HTLS11/150) (requires element HTLS150/150C-TARC).
  • Cylinder Drag Model (HTLS12/150) (requires element HTLS150/150C-TARC).
  • Paraboloid Drag Model (HTLS13/150) (requires element HTLS150/150C-TARC).
  • Dimpled Sphere Drag Model (HTLS14/150) (requires element HTLS150/150C-TARC).
  • Wing Drag Model (HTLS15/150) (requires element HTLS150/150C-TARC).
  • Airplane Drag Model (HTLS16/150) (requires element HTLS150/150C-TARC).
  1. Measurement of hydrodynamic drag and lift forces in different models:
  • Sphere Drag Model (HTLS7/150) (requires element HTLS150/150C-TARC).
  • Hemisphere Drag Model (HTLS8/150) (requires element HTLS150/150C-TARC).
  • Circular Plate Drag Model (HTLS9/150) (requires element HTLS150/150C-TARC).
  • Ring Drag Model (HTLS10/150) (requires element HTLS150/150C-TARC).
  • Square Plate Drag Model (HTLS11/150) (requires element HTLS150/150C-TARC).
  • Cylinder Drag Model (HTLS12/150) (requires element HTLS150/150C-TARC).
  • Paraboloid Drag Model (HTLS13/150) (requires element HTLS150/150C-TARC).
  • Dimpled Sphere Drag Model (HTLS14/150) (requires element HTLS150/150C-TARC).
  • Wing Drag Model (HTLS15/150) (requires element HTLS150/150C-TARC).
  • Airplane Drag Model (HTLS16/150) (requires element HTLS150/150C-TARC).
  1. Study of static pressure, dynamic pressure and total pressure with the Pitot tube (HTLS11/150).
  2. Study of the static pressure, dynamic pressure and total pressure with the Wake Survey Rake (HTLS12/150).

Other possibilities to be done with this unit:

  1. Many students view results simultaneously. To view all results in real time in the classroom by means of a projector or an electronic whiteboard.
  2. Open Control, Multicontrol and Real Time Control. This unit allows intrinsically and/or extrinsically to change the span, gains, proportional, integral, derivate parameters, etc, in real time.
  3. The Computer Control System with SCADA and allow a real industrial simulation.
  4. This unit is totally safe as uses mechanical, electrical and electronic, and software safety devices.
  5. This unit can be used for doing applied research.
  6. This unit can be used for giving training courses to Industries even to other Technical Education Institutions.
  7. Control of the HTLS150/150C unit process through the control interface box without the computer.
  8. Visualization of all the sensors values used in the HTLS150/150C unit process.
  9. Several other exercises can be done and designed by the user.

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