The drag characteristics for a newly designed automobile having a maximum characteristic length of \(20 \mathrm{ft}\) are to te determined through a model study, The characteristics at both low speed (approximately \(20 \mathrm{mph}\) ) and high speed \((90 \mathrm{mph})\) are of interest. For a series of projected model tests, an unpressurized wind tunnel that will accommodate a model with a maximum characteristic length of \(4 \mathrm{ft}\) is to be used. Determine the range of air velocities that would be required for the wind tunnel if Reynolds number similarity is desired. Are the velocities suitable? Explain.

Short Answer

Expert verified
The wind tunnel would need to produce air speeds of 100 mph and 450 mph to simulate the car moving at low speed (20 mph) and high speed (90 mph), respectively. The low speed characteristics can be studied using a regular wind tunnel but the high speed conditions cannot due to the excessively high required speed.

Step by step solution

01

Derive the formula for velocity ratio

Since the Reynolds number for the model and the real car should be the same, we have \(Re_{\text{car}} = Re_{\text{model}} \) which leads to \(\frac{ρV_{\text{car}}d_{\text{car}}}{μ} = \frac{ρV_{\text{model}}d_{\text{model}}}{μ}\). After simplification, we can see that the ratio of the velocities, \(V_{\text{model}} / V_{\text{car}}\), should be equal to the ratio of the lengths, \(d_{\text{car}} / d_{\text{model}}\). This equation can then be solved for the model's velocity, \(V_{\text{model}}\), to get \(V_{\text{model}} = V_{\text{car}} * (d_{\text{car}} / d_{\text{model}})\).
02

Calculate wind tunnel velocities needed for low speed and high speed characteristics

To determine the velocities required for the wind tunnel, we use the formula derived in Step 1. The characteristic dimension ratio \(d_{\text{car}} / d_{\text{model}}\) is 20ft/4ft, which is 5. Using this, the model velocities for low speed (\(20 \, \text{mph}\)) and high speed (\(90 \, \text{mph}\)) conditions can be calculated as such: \(V_{\text{model, low speed}} = 20 \, \text{mph} * 5 = 100\, \text{mph}\) and \(V_{\text{model, high speed}} = 90 \, \text{mph} * 5 = 450 \, \text{mph}\)
03

Evaluate feasibility of the calculated velocities

Typically, wind tunnels can generate air speeds up to about 100 mph. We find that the calculated velocity for the low speed characteristics, \(100 \, \text{mph}\), is possible to achieve in a wind tunnel. However, the value of \(450 \, \text{mph}\) for the high speed conditions is not achievable in regular wind tunnels and could, realistically, only be achieved in a high-speed wind tunnel. Therefore, while the low speed characteristics can be studied through the model study, the high speed characteristics would likely not be feasible.

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 Vaia!

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

The dimensional parameters used to describe the operation of a ship or airplane propeller (sometimes called a screw propeller) are rotational speed, \(\omega,\) diameter, \(D,\) fluid density, \(\rho\) speed of the propeller relative to the fluid, \(V\), and thrust developed, \(T .\) The common dimensionless groups are called the thrust coefficient and the advance ratio. Propose appropriate definitions for these groups.

For a certain fluid flow problem it is known that both the Froude number and the Weber number are important dimensionless parameters. If the problem is to be studied by using a 1: 15 scale model, determine the required surface tension scale if the density scale is equal to \(1 .\) The model and prototype operate in the same gravitational field.

The fluid dynamic characteristics of an airplane flying \(240 \mathrm{mph}\) at \(10,000 \mathrm{ft}\) are to be investigated with the aid of a 1: 20 scale model. If the model tests are to be performed in a wind tunnel using standard air, what is the required air velocity in the wind tunnel? Is this a realistic velocity?

An incompressible fluid oscillates harmonically \(\left(V=V_{0}\right.\) \(\sin \omega t, \text { where } V \text { is the velocity })\) with a frequency of 10 rad/s in a 4-in.- -diameter pipe. A \(\frac{1}{4}\) scale model is to be used to determine the pressure difference per unit length, \(\Delta p_{\ell}\) (at any instant) along the pipe. Assume that $$\Delta p_{\ell}=f\left(D, V_{0}, \omega, t, \mu, \rho\right)$$ where \(D\) is the pipe diameter, \(\omega\) the frequency, \(t\) the time, \(\mu\) the fluid viscosity, and \(p\) the fluid density. (a) Determine the similarity requirements for the model and the prediction equation for \(\Delta p_{\ell}\) (b) If the same fluid is used in the model and the prototype at what frequency should the model operate?

The pressure rise, \(\Delta p,\) across a pump can be expressed as \\[ \Delta p=f(D, \rho, \omega, Q) \\] where \(D\) is the impeller diameter, \(\rho\) the fluid density, \(\omega\) the rotational speed, and \(Q\) the flowrate. Determine a suitable set of dimensionless parameters.

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.

Sign-up for free