/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 55 The drag on a small, completely ... [FREE SOLUTION] | 91Ó°ÊÓ

91Ó°ÊÓ

The drag on a small, completely submerged solid body having a characteristic length of \(2.5 \mathrm{mm}\) and moving with a velocity of \(10 \mathrm{m} / \mathrm{s}\) through water is to be determined with the aid of a model. The length scale is to be \(50,\) which indicates that the model is to be larger than the prototype. Investigate the possibility of using either an unpressurized wind tunnel or a water tunnel for this study. Determine the required velocity in both the wind and water tunnels and the relationship between the model drag and the prototype drag for both systems. Would either type of test facility be suitable for this study?

Short Answer

Expert verified
Calculate Reynolds numbers and use them for velocity requirements in both tunnels. Compare model drag with prototype drag based on dynamic similarity.

Step by step solution

01

Understand the Problem

We need to determine the velocities required in a wind tunnel and a water tunnel to simulate the drag on a prototype using a larger model. The model is scaled up with a length scale of 50, which means the model is 50 times larger than the prototype. We will explore both wind and water tunnel options.
02

Determine Reynolds Number for Prototype

The Reynolds number (Re) for the prototype must be calculated since it is a dimensionless number that reflects the ratio of inertial forces to viscous forces and is crucial for dynamic similarity. For the prototype, use the formula \[Re_{p} = \frac{\rho_{water} \times V_{p} \times L_{p}}{\mu_{water}}\]where:- \(\rho_{water}\) is the density of water- \(V_{p} = 10 \text{ m/s}\) is the velocity of the prototype- \(L_{p} = 2.5 \times 10^{-3} \text{ m}\) is the characteristic length of the prototype- \(\mu_{water}\) is the dynamic viscosity of water

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with 91Ó°ÊÓ!

Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Reynolds number
The Reynolds number is a key parameter in fluid mechanics, essential for predicting different flow patterns. It is a dimensionless number that compares inertial forces to viscous forces in a fluid. This concept is critical for understanding whether a flow will be laminar or turbulent. In the context of the exercise, calculating the Reynolds number for the prototype helps in ensuring that the model test conditions match the real-world behavior.For the prototype submerged in water, the Reynolds number can be calculated using the formula:\[ Re = \frac{\rho \times V \times L}{\mu} \]Where:- \( \rho \) is the fluid density- \( V \) is the fluid velocity relative to the object- \( L \) is the characteristic length- \( \mu \) is the dynamic viscosity of the fluidDetermining its value ensures that the experiment's dynamic similarity is upheld. It captures how velocity, viscosity, and object size interplay, influencing how fluids behave around different objects.
dynamic similarity
Dynamic similarity is a concept used in fluid mechanics to predict the behavior of fluids interacting with objects. It involves creating a model that accurately reflects the fluid dynamics experienced by the actual prototype but in a scaled-down or scaled-up manner. To achieve dynamic similarity between the prototype and the model: - The Reynolds number of the model must be equal to that of the prototype. - This ensures the fluid flow characteristics (like turbulence and drag) are similar, making the study results applicable to real-world scenarios. By ensuring dynamic similarity, engineers can experimentally measure forces or other effects on a scale model and then confidently translate these observations to predict the behavior on the actual full-scale prototype.
drag force
Drag force is the resistance force caused by the motion of a body through a fluid, like air or water. This force opposes the object’s direction of motion and is crucial for designing vehicles, airplanes, and marine vessels to optimize energy efficiency.Drag can be calculated using:\[ F_d = \frac{1}{2} C_d \rho A V^2 \]Where:
  • \( F_d \) is the drag force
  • \( C_d \) is the drag coefficient, which depends on the shape of the object
  • \( \rho \) is the fluid density
  • \( A \) is the reference area, usually the projected frontal area of the object
  • \( V \) is the velocity of the object through the fluid
Understanding drag is crucial. It plays a significant role in many engineering applications, from designing airplanes that consume less fuel to understanding how to build faster ships.
wind tunnel
Wind tunnels are large tubes with air moving inside. Scientists and engineers use wind tunnels to test the effects of air moving on or around solid objects, such as airplanes, cars, or even small-scale models. Key points about wind tunnels: - They help simulate real-world conditions by controlling air flow around an object to study aerodynamics. - Parameters like speed, air pressure, and turbulence can be controlled to study different conditions. In this exercise, using a wind tunnel involves adjusting the velocity to ensure the Reynolds number matches that of the water-bound prototype. This allows engineers to observe and measure how different designs perform and optimize them for better performance.
water tunnel
Similar to wind tunnels, water tunnels are used to study the interactions of water flow with submerged objects. They are vital in marine engineering and other fields that involve large bodies of water, like shipbuilding. Key features of water tunnels include:
  • They allow detailed observation of water flow over models.
  • Speed, turbulence, and pressure conditions are adjustable to simulate various conditions.
  • They help in predicting the performance of aquatic vehicles and structures.
In the context of this exercise, the water tunnel must replicate the fluid flow conditions of the smaller prototype in water. Achieving the same Reynolds number ensures that the results are valid and can be used for practical applications or further studies.

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Assume that the drag, \(\mathscr{D},\) on an aircraft flying at supersonic speeds is a function of its velocity, \(V\), fluid density, \(\rho\) speed of sound, \(c,\) and a series of lengths, \(\ell_{1}, \ldots, \ell_{i},\) which describe the geometry of the aircraft. Develop a set of pi terms that could be used to investigate experimentally how the drag is affected by the various factors listed. Form the pi terms by inspection.

7.62 A thin rectangular plate is towed through seawater at an average velocity of 5 mph. The plate is held in a vertical position and projects above the undisturbed level of the water to a height \(z . A 1: 4\) scale model is to be used to predict the drag on the plate, and the model fluid is also seawater. (a) Assuming that Froude number similarity must be maintained, determine the required model velocity. (b) What is the required value of \(z_{m} / z ?\) (c) A measured drag of 1 lb on the model will correspond to what drag on the prototype?

Under certain conditions, wind blowing past a rectangular speed limit sign can cause the sign to oscillate with a frequency \(\omega\). (See Fig. P7.11 and Video Y9.6.) Assume that \(\omega\) is a function of the sign width, \(b\), sign height, \(h\), wind velocity, \(V\), air density, \(\rho\), and an elastic constant, \(k\), for the supporting pole. The constant, \(k\), has dimensions of \(F L\). Develop a suitable set of pi terms for this problem.

Assume that the flowrate, \(Q\), of a gas from a smokestack is a function of the density of the ambient air, \(\rho_{n}\), the density of the gas, \(\rho_{8}\), within the stack, the acceleration of gravity, \(g\), and the height and diameter of the stack, \(h\) and \(d\), respectively. Use \(\rho_{a}, d\) and \(g\) as repeating variables to develop a set of pi terms that could be used to describe this problem.

The drag characteristics of an airplane are to be determined by model tests in a wind tunnel operated at an absolute pressure of \(1300 \mathrm{kPa}\). If the prototype is to cruise in standard air at \(385 \mathrm{km} / \mathrm{hr},\) and the corresponding speed of the model is not to differ by more than \(20 \%\) from this (so that compressibility effects may be ignored), what range of length scales may be used if Reynolds number similarity is to be maintained? Assume the viscosity of air is unaffected by pressure, and the temperature of air in the tunnel is equal to the temperature of the air in which the airplane will fly.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.