Air Volume Flow Rate and Centerline Velocity in a Tube Wind Tunnel

Slides:



Advertisements
Similar presentations
S. Ghosh, M. Muste, M. Marquardt, F. Stern
Advertisements

ME 322: Instrumentation Lecture 15
Applications of Bernoulli’s Equation What happens if the bicyclist is accelerating or decelerating? Figure E3.2 (p. 101)
Elementary Mechanics of Fluids
Fluid in Motion.
Pitot Stagnation Tubes Under Laminar Conditions *P7.24 Jace Benoit February 15, 2007.
Determination of Vacuum Pump Operational Efficiency By: D K Singhal Chandpur Enterprises Ltd. 1.
Study of Liquid Breakup Process in Solid Rocket Motors Author: Michael Stefik & Bryan Sinkovec, Co-Author: Yi Hsin Yen, Faculty Advisor: Professor Ryoichi.
10. Measurement of Air Quantities and Pressure Differences.
ME 388 – Applied Instrumentation Laboratory Wind Tunnel Lab
CHE/ME 109 Heat Transfer in Electronics LECTURE 18 – FLOW IN TUBES.
Wind Instrument Testing Apparatus Project WITAP Team: Rob Koch Andy Lawrence.
Slides for ME 115 Laboratory Wind tunnels Purposes –To provide a uniform velocity field (e.g. aeronautic, automotive testing) and low turbulence intensity.
 Purpose  Test design  Measurement system and Procedures  Uncertainty Analysis.
Introduction to Fluid Mechanics
Flow Sensors.
Hydrodynamics.
Measuring Lower and Upper Atmospheric Conditions By: Ashley Noah.
Fluid Mechanics 05.
CHE/ME 109 Heat Transfer in Electronics
ME 322: Instrumentation Lecture 16 February 25, 2015 Professor Miles Greiner Lab 6 calculations (Excel demo)
Assignment No. 1 [Grup 8] Figure below shows a portion of a hydraulic circuit. The pressure point B must be 200 psig when the volume flow rate is 60 gal/min.
Practical Aspects of using Pitot Tube
Flow Measurement Muhajir Ab. Rahim School of Mechatronic Engineering
Chapter 2, Lesson 3.  A weather forecast is a prediction of weather conditions over the next 3 to 5 days.  A meteorologist is a person who observes.
Measurement of Pressure Distribution and Lift for an Airfoil  Purpose  Test design  Measurement system and Procedures  Instrumentation  Data reduction.
Add To Table of Contents:
 Purpose  Test design  Measurement system and Procedures  Uncertainty Analysis.
Cost-effectiveness: An Engineers's Real Job Problem 3.138* Created By: Patrick Thomas.
ME 322: Instrumentation Lecture 11 February 11, 2015 Professor Miles Greiner Pitot probe operation, non-linear transfer function, fluid density, uncertainty,
Copyright: Prof S.A. Kinnas
ME 322: Instrumentation Lecture 13: Exam Review February 18, 2015 Professor Miles Greiner.
Measurement of Pressure Distribution and Lift for an Airfoil  Purpose  Test design  Measurement system and Procedures  Uncertainty Analysis  Data.
Lab 3 Static Calibration of Manometers Using Electronic Pressure Transmitters Lab Instructor: A. Sunkara Performed: January 27, 2005, 10 AM Miles Greiner.
Height Differences Using Flat-Plate Boundary Layer Problem 7.24* Pamela Christian BIEN 301 Individual Project February 15, 2007.
MECH 322 Instrumentation Lab 5 Elastic Modulus of an Aluminum Beam Performed: February 9, 2004 Sinan Ozcan: I believe I performed 50% of the work for this.
What are they? What do they do?
ME 322 LAB 7 Computer Data Acquisition System for Steady Thermocouple Signals Performed : 02/13/2004 Sinan Ozcan : I believe I performed 50% of this lab.
MECH 322 Instrumentation Lab 6 Fluid Speed and Volume Flow Rate Performed: February 27, 2007 Group 0 Miles Greiner Lab Instructors: Mithun Gudipati, Venkata.
ME 391 Instrumentation LAB #6 Volume Flow Rate and Centerline Speed in a Tube Wind Tunnel Performed: 03/05/2004 Soma: I believe I performed 50% of this.
Wind and Water Power pp Wind generators  Horizontal Axis— higher positioning of rotor blades  Vertical Axis— catches wind closer to the ground.
Introduction to Fluid Mechanics
Experiment #1: Centrifugal Pumps Alberto J.Pérez #79737.
Physical Modeling of the Atmospheric Boundary Layer in the UNH Flow Physics Facility Stephanie Gilooly and Gregory Taylor-Power Advisors: Dr. Joseph Klewicki,
SUGGESTED MINIMUM KNOWLEDGE OF FLUID MECHANICS AND FOR FE EXAM
MECH 391 Instrumentation Lab 11 Unsteady Velocity in a Karman Vortex Street Performed: 04/07/05 Sinan Ozcan: I believe I performed 50% of this lab Participation.
UNDERSTANDING DIFFERENT
What are they? What do they do?
2D Free Jet Simulations (FLUENT)
Process Variables, Elements and Instruments – Flow - Agenda
Figure 10.1 Flow in a duct with area change.
Internal Incompressible
alternate form of Euler’s equation
General Information Lab -3 Bernoulli Equation
ME 322: Instrumentation Lecture 16
ME 391 LAB#5 Construction of a Computer Data Acquisition System for Measuring Steady Thermocouple Signals Performed : 02/13/2004 Sinan Ozcan : I believe.
ME 391 Instrumentation Lab 10 Calibration of a Hot-Film Anemometer
LAB #6 Volume Flow Rate and Centerline Speed in a Tube Wind Tunnel
Slides for ME 115 Laboratory
S. Ghosh, M. Muste, M. Marquardt, F. Stern
Venturi Effect The Venturi effect is named after an Italian Physicist; Giovanni Venturi (1746–1822). The Venturi Effect is the reduction in fluid pressure.
What are they? What do they do?
Characterization of Inlet Contamination Potential
What are they? What do they do?
What are they? What do they do?
Projectile Motion Free fall with an initial horizontal velocity
Fluid flow A fluid is a substance that flows When subjected to a shearing stress layers of the fluid slide relative to each other Both gases and liquids.
Frog What angle is the frog jumping at? Why does this make sense?
Introduction to Fluid Mechanics
Presentation transcript:

Air Volume Flow Rate and Centerline Velocity in a Tube Wind Tunnel ME 391 Instrumentation LAB # 7 Air Volume Flow Rate and Centerline Velocity in a Tube Wind Tunnel Performed: 03/05/2004 Soma : I believe I performed 50% of this lab. Sinan Ozcan: I believe I performed 50% of this lab.

Abstract The volumetric flow rate and centerline velocity of air in a tube wind tunnel were measured for a range of blower speeds. As a consistency check, the centerline speed for each flow rate was compared to the centerlines speed that would be predicted from slug and parabolic velocity profiles. The volume flow rate and centerline speed were determined by measuring the pressure signal across venturi tube and a Pitot probe. Vertical and inclined manometers were used to measure these pressure drops. The maximum volume flow rate was 0.077 + 0.002 m3/s. The measured centerline velocity was bracketed by the values predicted for slug and parabolic velocity for all blower speeds. At the lowest blower speed, the measured centerline speed is closer to the value predicted for laminar flow than it is at higher speeds. By observation we conclude that uncertainty is small when blower inlet is closed compared to the blower inlet is open.

Table 1 Atmospheric Pressure and Temperature Readings

Table 2 Measurement Readings and Calculated Values This table presents the vertical and inclined manometer readings for the gage pressure, the venturi tube, and the pitot probe, for different blower speeds. The uncertainty of each reading is also included. The calculated volume flow rate, centerline velocity and their uncertainties are also tabulated. The uncertainties from the inclined manometer are smaller than those from the vertical manometer. From the above table we can infer that Uncertainty is small when the blower inlet is closed than the blower inlet is open.

Figure 1 Measured and Predicted Centerline Velocities Versus Volume Flow Rate The measured centerline velocity is between the values predicted for slug and parabolic velocity. At the lowest blower speed, the measured centerline speed is closer to the value predicted for laminar flow than it is at higher speeds