(a)
The deflection under load.
(a)
Answer to Problem 3.48P
The deflection under load is
Explanation of Solution
Given:
The length of the beam is
The mass of the beam is
The diameter of the shaft is
Formula used:
The expression for the load is given as,
Here,
The expression for the moment of inertia of the shaft is given as,
The expression for the deflection is given as,
Here,
Calculation:
The value of load can be calculated as,
The value of moment of inertia of the shaft can be calculated as,
The value of young’s modulus of AISI 303 steel is
The value of deflection can be calculated as,
Conclusion:
Therefore, the deflection under load is
(b)
The diameter of the shaft made from 2024-T4 aluminum.
The diameter of the shaft made from architectural bronze.
The diameter of the shaft made from 99.5% titanium.
(b)
Answer to Problem 3.48P
The diameter of the shaft made from 2024-T4 aluminum is
The diameter of the shaft made from architectural bronze is
The diameter of the shaft made from 99.5% titanium is
Explanation of Solution
Calculation:
The value of young’s modulus of 2024-T4 aluminum is
The value of moment of inertia of the shaft made from 2024-T4 aluminum can be calculated as,
The value of the diameter of the shaft made from 2024-T4 aluminum can be calculated as,
The value of young’s modulus of architectural bronze is
The value of moment of inertia of the shaft made from architectural bronze can be calculated as,
The value of the diameter of the shaft made from architectural bronze can be calculated as,
The value of young’s modulus of 99.5% titanium is
The value of moment of inertia of the shaft made from 99.5% titanium can be calculated as,
The value of the diameter of the shaft made from 99.5% titanium can be calculated as,
Conclusion:
Therefore, the diameter of the shaft made from 2024-T4 aluminum is
Therefore, the diameter of the shaft made from architectural bronze is
Therefore, the diameter of the shaft made from 99.5% titanium is
Want to see more full solutions like this?
Chapter 3 Solutions
EBK MANUFACTURING PROCESSES FOR ENGINEE
- M=E/p². (b) Show that the lightest cantilever beam of length L and square section (area free) that will not deflect by more than 8 under an end load F is that made of the material with the largest value of M = Ep (neglect self-weight). loungs modulusE GPa Plot each index on the given (E- p) chart indicating the search area for materials with the highest values of each. 1000 HINT: Start each of the problem by listing the function, the objective and the constraints. You will need the equations for the deflection of a cantilever beam with a square cross-section t x t. You can either derive the equations or use the equations provided in Appendix B, Section B3. 100 10 1 10-1 10-2 Loungs modulus density 10-4 Longitudinal wave speed 10 ms 3x10² Foams. 10 ms- 10-3 3x10² Rigid polymer foams 10 ms Technical ceramics Al alloys Composites CFRP Glass Bamboo Mg alloys GFRP Wood Flexible polymer foams Natural PMMA- materials PA grain Cork PS Wood grain Leat e EVA Isoprene Buty rubber B4C. Polyester…arrow_forwardConsider the simply supported beam shown in (Egure 1) E 200 GPa and I-80.0(10) mm² Figure 2m 30 KN 2 m 15 KN 1 of 1 Previous Figure Part A Determine the maximum deflection of the beam Express your answer to three significant figures and include the appropriate ut displacement is upward and negative value if the displacement is downward. Unax Submit HA Value Provide Feedback Request Answer Units ?arrow_forwardA bar having a circular cross section is carrying a tensile load of 30 kN. If the diameter and length of the bar are 6 mm and 80 cm respectively, calculate the deflection. Assume Young’s modulus is 207 GPaarrow_forward
- (b) Figure 1 shows the S-N fatigue figure curve for nickel-based alloy beam. The beam is subjected to a cyclical load of 100 N with equal maximum and minimum stresses. The diameter of the beam is 5 mm and length is 50 mm long. Evaluate: (i) The lifetime of the beam in number of cycles to failure (ii) The lifetime in hour if the cycle frequency is set to 10 Hz 70 65 450 60 400 55 350 45 300 40 250 35 30 105 106 107 10 Cycles to failure Figure 1: The S-N fatigue curve for a nickel alloy. Stress (ksi) Sress (MPa)arrow_forwardA horizontal steel I – beam of cross-sectional area 0.041m2 is rigidly connected to two vertical girders. If the beam was installed when the temperature was 300C, what stress is developed in the beam when the temperature drops to - 300C? (b) Is the ultimate strength of the steel exceeded? (c)What stress is developed if the beam is concrete and has a cross- sectional area of 0.13m2 ? Will it fracture?arrow_forward(1) The belt tension in a 400mm pulley is 4,000N. It is mounted to a shaft to transmit power to another pulley 250mm away. The solid steel shaft has yield strength of 250MPa. Determine: (a) the minimum diameter of the shaft to be used; (b) the angular deflection if modulus of rigidity is 90GPa.arrow_forward
- How are the energy methods applied in order to solve problems involving deflection?arrow_forwardWhat is the minimum thickness of a normal weight concrete cantilever slab with length of 2.96 m and steel yield strength of 356 MPa?arrow_forwardTwo long columns A and B are made of same material, and also have the same length.The cross section of column A is square and column B is circular. If both columns have thesame amount of cross sectional area, then which column will carry more compressiveload? Justify your answer with engineering analysis. Assume both columns have fixed-fixedend supports. What is engineering of application of this solution? Discuss briefly.arrow_forward
- A cylindrical rod 380 mm long and having a diameter of 10.0 mm is to be deformed using a tensile load of 22 KN. It must not experience either plastic deformation or a diameter reduction of more than 0.01 mm. Of the materials listed as follows, which are possible candidates? Show your solution Aluminum E-70GPa, Yield Strength 255 MPa, Poisson's ration 0.33 Brass E=105GPa, Yield Strength 345 MPa, Poisson's ration 0.34 Steel E=207GPa, Yield Strength 450 MPa, Poisson's ration 0.30 Copper E=110GPa, Yield Strength 250 MPa, Poisson's ration 0.33arrow_forwardDiscuss the deflection caused by shear stress?arrow_forwardUsing the previous answers; determine the angular deflection in both shafts. Both shafts are 20 cm long and the modulus of rigidity for the material is 60GN/m^2.arrow_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