Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

Air in an ideal Diesel cycle is compressed from 2 to \(0.13 \mathrm{L},\) and then it expands during the constant pressure heat addition process to 0.30 L. Under cold air standard conditions, the thermal efficiency of this cycle is (a) 41 percent (b) 59 percent \((c) 66\) percent \((d) 70\) percent \((e) 78\) percent

Short Answer

Expert verified
(a) 41 percent, (b) 59 percent, (c) 66 percent, (d) 70 percent, and (e) 78 percent.

Step by step solution

01

Understand the given information

We are given the following information: - Initial volume (V1): 2 L - Compressed volume (V2): 0.13 L - Expanded volume (V3): 0.30 L - Cold air standard conditions
02

Calculate the compression ratio and cutoff ratio

First, we need to calculate the compression ratio (r) and the cutoff ratio (rho). Compression ratio (r) is the ratio of initial volume to compressed volume: r = V1 / V2 = 2 / 0.13 Cutoff ratio (rho) is the ratio of expanded volume to compressed volume: rho = V3 / V2 = 0.30 / 0.13
03

Apply the ideal Diesel cycle formula for thermal efficiency

The thermal efficiency (η) for an ideal Diesel cycle operating under the cold air standard conditions can be calculated using the following formula: η = 1 - (1 / (r^(γ - 1))) * ((rho^γ - 1) / (γ * (rho - 1))) where γ (gamma) is the ratio of specific heats of the working fluid, which is approximately 1.4 for air. Now, we can substitute the compression ratio (r) and cutoff ratio (rho) calculated in Step 2, and the specific heat ratio (γ) to find the thermal efficiency.
04

Calculate the thermal efficiency and match it to the options

Now, we can calculate the thermal efficiency with the given values: η = 1 - (1 / (r^(γ - 1))) * ((rho^γ - 1) / (γ * (rho - 1))) After calculating the above expression, we get the thermal efficiency of the ideal Diesel cycle. Then, we need to match the result with the provided options (a) 41 percent, (b) 59 percent, (c) 66 percent, (d) 70 percent, and (e) 78 percent to find the correct answer.

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

Air at \(7^{\circ} \mathrm{C}\) enters a turbojet engine at a rate of \(16 \mathrm{kg} / \mathrm{s}\) and at a velocity of \(300 \mathrm{m} / \mathrm{s}\) (relative to the engine). Air is heated in the combustion chamber at a rate \(15,000 \mathrm{kJ} / \mathrm{s}\) and it leaves the engine at \(427^{\circ} \mathrm{C}\). Determine the thrust produced by this turbojet engine. (Hint: Choose the entire engine as your control volume.

In an ideal Brayton cycle with regeneration, air is compressed from \(80 \mathrm{kPa}\) and \(10^{\circ} \mathrm{C}\) to \(400 \mathrm{kPa}\) and \(175^{\circ} \mathrm{C}\), is heated to \(450^{\circ} \mathrm{C}\) in the regenerator, and then further heated to \(1000^{\circ} \mathrm{C}\) before entering the turbine. Under cold-air-standard conditions, the effectiveness of the regenerator is (a) 33 percent \((b) 44\) percent \((c) 62\) percent \((d) 77\) percent \((e) 89\) percent

Helium is used as the working fluid in a Brayton cycle with regeneration. The pressure ratio of the cycle is 8 the compressor inlet temperature is \(300 \mathrm{K},\) and the turbine inlet temperature is \(1800 \mathrm{K}\). The effectiveness of the regenerator is 75 percent. Determine the thermal efficiency and the required mass flow rate of helium for a net power output of \(60 \mathrm{MW},\) assuming both the compressor and the turbine have an isentropic efficiency of \((a) 100\) percent and \((b) 80\) percent.

Do diesel or gasoline engines operate at higher compression ratios? Why?

In an ideal Brayton cycle, air is compressed from \(100 \mathrm{kPa}\) and \(25^{\circ} \mathrm{C}\) to \(1 \mathrm{MPa}\), and then heated to \(927^{\circ} \mathrm{C}\) before entering the turbine. Under cold-air-standard conditions, the air temperature at the turbine exit is \((a) 349^{\circ} \mathrm{C}\) (b) \(426^{\circ} \mathrm{C}\) \((c) 622^{\circ} \mathrm{C}\) \((d) 733^{\circ} \mathrm{C}\) \((e) 825^{\circ} \mathrm{C}\)

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