Preview

Impact of Jet

Best Essays
Open Document
Open Document
2091 Words
Grammar
Grammar
Plagiarism
Plagiarism
Writing
Writing
Score
Score
Impact of Jet
1.0 ABSTRACT
The purpose of the impact of jet experiment is to design a system to determine the force generated by the impact of jet on a variety of target vanes. A formula is given to calculate the reaction force at the different vanes caused by the jet. At the end of the experiment, the data collected and results calculated will then be compared to theoretical values which are given. Students are expected to be able to come to a conclusion regarding the relationship between the reaction force produced at the target vanes and the angle where the shape of the vanes curve.

1.1 INTRODUCTION There are many ways to produce mechanical work from fluid under pressure. One of the famous ways is to use the pressure to accelerate the fluid to a high velocity in a jet. Over the years, engineers have found many ways to utilize the force that can be produced by a jet of fluid on a surface diverting the flow. For example, the pelton wheel has been used to make flour. Firemen make use of the kinetic energy stored in a jet to deliver water above the level in the nozzle to extinguish fires in tall buildings. Fluid jets are also used in industry for cutting metals and debarring. This goes to show the importance of applications of the fluid jet in the technological aspects of various fields in our society. This experiment aims at assessing the different forces exerted by the same water jet on a variety of geometrically different plates. A ‘jet impact apparatus’ is used to carry out this experiment whereby three vanes of different geometrical properties are used. The results obtained experimentally are to be compared with the ones inferred from theory through utilizing the applicable versions of the Bernoulli and momentum equations.

2.0 EXPERIMENTAL DESIGN

2.1 MATERIALS

1. The Jet Impact Apparatus ( as shown in the figure ) 2. Volumetric Hydraulic Bench/Water 3. 3 different shape of vanes; Flat Plate, Conical Cup, and Hemispherical Cup 4.



References: * Massey, B.S. (1989). Mechanics of Fluids. 6th Ed, Chapman & Hall. * White F.M.(1994). Fluid Mechanics. 3rd Ed., McGraw-Hill. * Van Dyke M.(1982).An Album of Fluid Motion. Parabolic Press. * Coulson, J.M.; and Richardson, J.F. Chemical Engineering, Volume 1. 6th Ed.,Butterworth-Heinemann. * web.cecs.pdx.edu.(No date). Impact of A Jet. Available at: http://web.cecs.pdx.edu/~gerry/class/EAS361/lab/pdf/lab4_impactOfJet.pdf [Accessed 15 May 2013] * codecogs.com. (No date). Impact of jets. Available at: http://www.codecogs.com/reference/engineering/fluid_mechanics/jet/impact_of_jets.php [Accessed 15 May 2013] * http://staff.fit.ac.cy. (No date). Impact of A Jet. Available at: http://staff.fit.ac.cy/eng.fm/classes/amee202/Fluids%20Lab%20Impact%20of%20a%20Jet.pdf [Accessed 15 May 2013]

You May Also Find These Documents Helpful

  • Better Essays

    As a result of the experiment and computation of data, the aerofoil was found to have a critical Mach number of M=0.732. Below this freestream Mach number the Prandtl-Glauert law predicted results very successfully. However, above this value, the law completely breaks down. This was found to be the result of local regions of supersonic flow and local shockwaves.…

    • 2069 Words
    • 9 Pages
    Better Essays
  • Satisfactory Essays

    10. Force of impact- Force of impact would be the speed of the vehicle when it hits something.…

    • 360 Words
    • 2 Pages
    Satisfactory Essays
  • Better Essays

    In this experiment in a low speed flow the static pressure around an aerofoil will be observed and discussed. The lift on the aerofoil will also be calculated and compared with the theoretical value. The aerofoil being used in this particular experiment is symmetrical and is taking place in a wind tunnel with a speed of 18.5m/s, therefore the flow is assumed to be incompressible. The different pressures along the surface of the aerofoil will be measured at an angle of attack of 4.1 degrees and 6.2 degrees. These values of pressure will then be analysed and graphs and calculations will be produced, the lift being calculated using the trapezium method in excel and these values and graphs will then be compared to the theoretical results for an inviscid flow from the thin aerofoil theory. The errors in the experiment will be quantified and any improvements to the experiment will be discussed.…

    • 2962 Words
    • 12 Pages
    Better Essays
  • Better Essays

    introduction

    • 5346 Words
    • 41 Pages

    The aim of this experiment is to understand the non-linear aerodynamic characteristic of a slender wing-body (rocket shaped) by installing the slender wing-body inside the wing tunnel and run the wing tunnel at subsonic speed and changing the incidence angle of the slender from -14 to 28 degrees over period of time and record the lift and induced drag readings from a computer which is connected to the wind tunnel.…

    • 5346 Words
    • 41 Pages
    Better Essays
  • Satisfactory Essays

    Mass and Bowling Ball

    • 433 Words
    • 2 Pages

    Purpose: The purpose of this experiment is to determine if the weight of a certain object affects the velocity of the object when it hits the ground.…

    • 433 Words
    • 2 Pages
    Satisfactory Essays
  • Good Essays

    Fluids Mechanics

    • 694 Words
    • 3 Pages

    When a body or object moves, whether it be in air or water, it exerts a force and simultaneously encounters a resisting force from that medium.In sporting competitions such as swimming and athletics, drag and lift forces are constantly responding to the object or body’s thrust. There are many types of forces exerted by fluids that resist an implement or body trying to move through it. At the same time, technological improve- ments have enabled us to better use the specific fluid to decrease resistance; for example, better configuration of the dimples on a golf ball can improve its flight performance.…

    • 694 Words
    • 3 Pages
    Good Essays
  • Better Essays

    Physics of Airplanes

    • 1550 Words
    • 7 Pages

    Cited: Sanders. "AERODYNAMICS AND THEORY OF FLIGHT." Aerodynamics and Theory of Flight Langley Flying School. N.p., May 2008. Web. 19 Mar. 2013.…

    • 1550 Words
    • 7 Pages
    Better Essays
  • Good Essays

    Projectile Motion Lab

    • 1238 Words
    • 5 Pages

    * Take into account trial-to-trial variations in the velocity measurement when calculating the impact point.…

    • 1238 Words
    • 5 Pages
    Good Essays
  • Good Essays

    The aim of this practical is to build and evaluate the performance of a marble launcher, this is done by first finding the velocity of the marble using the equation v2=u2+2as, this will be done by conducting an experiment to first find the vertical distance (s) the marble travels and acceleration due to gravity (a).…

    • 1054 Words
    • 5 Pages
    Good Essays
  • Powerful Essays

    This paper introduces an experiment about launching a water rocket. The projectile motion of this water rocket will be examined.In this experiment,the water rocket will be launched at 4 different angles 30°,45°60°and 90 °.We will measure the ranges,maximum altitudes and air time in order to have a better understanding of the projectile motion.As the practical situation which includes the air resistance and different kinds of errors caused by students’ carelessness is different from the theory,it is unaviodable that the results are quite different from the theoretic statistics. The horizontal velocity is related to the range, while the vertical velocity is related to the maximum altitude. This experiment can help us reinforce the concepts related to the motion in two dimensions although the water rocket does not have the ideal situation. A lot of equations we learned in class can help our group calculate the range and maximum altitude.…

    • 1430 Words
    • 7 Pages
    Powerful Essays
  • Better Essays

    Hodanbosi, C. (1996). Pascal’s Principle and Hydraulics. Fairman, J. G. (Ed.) Retrieved from National Space and Aeronautics Administration, Glenn Research Center Web site: http://www.grc.nasa.gov/WWW/k-12/WindTunnel/Activities/Pascals_principle.html…

    • 1602 Words
    • 7 Pages
    Better Essays
  • Powerful Essays

    The aim of this experiment is to determine how the height of a horizontally launched projectile affects the projectiles range.…

    • 921 Words
    • 4 Pages
    Powerful Essays
  • Good Essays

    The purpose of this investigation is to measure the vertical displacement, or height of the launch, and the horizontal displacement, or range, travelled by a projectile (bullet from toy gun).…

    • 1404 Words
    • 6 Pages
    Good Essays
  • Good Essays

    Projectile Motion

    • 1093 Words
    • 5 Pages

    The purpose of this experiment is to be able to measure the velocity of a ball using two Photogates and computer software for timing, apply concepts from two-dimensional kinematics to predict the impact point of a ball in projectile motion and ability to understand trial-to-trial variations in the velocity measurement when calculating the impact point.…

    • 1093 Words
    • 5 Pages
    Good Essays
  • Powerful Essays

    DISCUSSION: The overlayed images of the pucks on the air hockey table show the progression of the pucks and the effect the collision had on them. Momentum is found by using the equation where p is momentum, m is mass and v is velocity. The law of the…

    • 1495 Words
    • 6 Pages
    Powerful Essays

Related Topics