Concept explainers
Complete each line of the following table on the basis of the conservation of energy principle for a closed system.
Qin kJ |
Wout kJ |
E1 kJ |
E2 kJ |
m kg |
e2 – e1 kJ/kg |
280 | — | 1020 | 860 | 3 | — |
−350 | 130 | 550 | — | 5 | — |
— | 260 | 300 | — | 2 | −150 |
300 | — | 750 | 500 | 1 | — |
— | −200 | — | 300 | 2 | −100 |
FIGURE P4–29
Fill the blanks from the below table on the basis of the conservation of energy principle for a closed system.
280 | 1020 | 860 | 3 | ||
130 | 550 | 5 | |||
260 | 300 | 2 | –150 | ||
750 | 500 | 1 | |||
300 | 2 |
Explanation of Solution
Write the energy balance equation for closed system.
Here, energy transfer in to the control volume is
Substitute
Here, amount of heat transfer into the system is
Substitute
Here, initial and final internal energy are
Conclusion:
For row I
Substitute
Substitute
For row II
Substitute
Substitute
For row III
Substitute
Substitute
For row IV
Substitute
Substitute
For row V
Substitute
Substitute
The following table blanks are filled and are shown below as summarized.
280 | 1020 | 860 | 3 | ||
130 | 550 | 5 | |||
260 | 300 | 2 | –150 | ||
750 | 500 | 1 | |||
300 | 2 |
Want to see more full solutions like this?
Chapter 4 Solutions
Thermodynamics: An Engineering Approach
- An element in plane stress is subjected to stresses ☐ x, y, and xx (see figure). Using Mohr's circle: a) Determine the principal stresses and the maximum in-plane shear stress acting at the point. b) Show these stresses in an appropriate sketch 12 MPa 27 MPa T 60 MPaarrow_forward5 kN-m A beam with an inverted tee-shaped cross section is subjected to positive bending mo- ments of M₂ = 5 kN-m. The cross-sectional dimensions of the beam are shown below. 10 mm Determine: (a) the centroid location, the moment of inertia about the z axis, 40 mm 5 kN-m K 150 mm H 15 mm 120 mm (b) the bending stress at points H and K. ans: 17.83mPa (c) the maximum bending stress produced in the cross section.arrow_forwardEXAMPLE 6.4 Draw the shear and moment diagrams for the beam shown in Fig. 6-7a. 15 kN 80 kN·m -5 m B -5 m (a) 5 kN/m Darrow_forward
- 2) A short rectangular post supports compressive loads of P- 175 kN and Q-90 kN, as shown in the figure below. A top view of the post showing the locations where loads P and Q are applied to the top of the post is also given. Determine the vertical normal stresses at corners a, b, c, and d of the post. P=175 kN Q=90 kN 160 mm 120 mm b 40 mm 160 mm a x d 60 mm 40 mmarrow_forwardFor the beam shown below: Find the equation for the shear force as function of x, V(x), along the x domains A-B (0 ≤ x ≤ 5 m) and B-C (5 m sxs 10 m), and draw the shear diagram for the beam. For each step, draw the associated free body diagram and indicate the equations of equilibrium used. Upload your answers in PDF. 2.5 m 15 kN 5 kN/m 80 kN·m Upload your D B 5m- ―5 marrow_forwardQ What is Theories of Brittle failure? Q, what do you mean for each of what's Coming? utں وہی رہیں > Tyiled , Puc > Sut, So, KP, Kt, q When to use this law. N= Out Ouc * Ouc 1 -Out (01+0₂) I'm a mechanical engineering student. I don't understand What is the difference ductile materials. between Brittle andarrow_forward
- Q2. (30 Marks) For the following figure: 1. Read the tolerances (GD&T) from the figure? 2. Write the Opitz code (5 digits only) for this product? 3. Write few points about point cloud? And how it can be used to inspect the geometry of products? 4. Draw sketch (free hand) to the top view of the figure below? (()) 5. For the symbol below the figure, what does it means? () will jo الهندسي 08±0.01 A 020±0.01 00.02MAM BM 010±0.01 00.02MAM ماذا يعني هذا Barrow_forwardQ: Find the steady-state response of the system shown in the figure below. Pulley, mass moment of inertia Jo 寻 k2 00000 For the following data: Fo sin of m 00000 uu x(t) w FO JO r m C k2 [Rad/s] [N] kg-m [cm] [Kg] [N.s/m] [N/m] kl [N/m] 28 58 1.8 13 18 540 540 1080arrow_forwardEx. Determine the safety factor for the bracket rod shown below for N = 6 x 107 Cycles. The notch radius at the wall is Y=0.25 cm.. the braket is made from Aluminum 2024, Cold-drawn with σy, 290 MP 441 MPa. L = 10 cm, a = 8 cm, d = 2cm. "Out = d Wall A rod arm a Farrow_forward
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY