(a)
The minimum weight of a
(a)
Answer to Problem 3.54P
The minimum weight of a
Explanation of Solution
Given:
The length of the wire is
The load supported by the member is
Formula used:
The expression for area of the specimen is given as,
Here,
The expression for mass of the specimen is given as,
Here,
Calculation:
Refer to table 3.4 “Room temperature mechanical properties and typical applications of annealed stainless steels” value obtained from this table is,
The expression for area of the specimen can be calculated as,
The expression for mass of the specimen can be calculated as,
Conclusions:
Therefore, the minimum weight of a
(b)
The minimum weight of a
(b)
Answer to Problem 3.54P
The minimum weight of a
Explanation of Solution
Given:
The length of the wire is
The load supported by the member is
Formula used:
The expression for area of the specimen is given as,
Here,
The expression for mass of the specimen is given as,
Here,
Calculation:
Refer to strength and density data book the value obtained as
The expression for area of the specimen can be calculated as,
The expression for mass of the specimen can be calculated as
Conclusions:
Therefore, the minimum weight of a
(c)
The minimum weight of a
(c)
Answer to Problem 3.54P
The minimum weight of a
Explanation of Solution
Given:
The length of the wire is
The load supported by the member is
Formula used:
The expression for area of the specimen is given as,
Here,
The expression for mass of the specimen is given as,
Here,
Calculation:
Refer to strength and density data book the value obtained as
The expression for the area of the specimen can be calculated as,
The expression for mass of the specimen can be calculated as
Conclusions:
Therefore, the minimum weight of a
(d)
The minimum weight of a
(d)
Answer to Problem 3.54P
The minimum weight of a
Explanation of Solution
Given:
The length of the wire is
The load supported by the member is
Formula used:
The expression for area of the specimen is given as,
Here,
The expression for mass of the specimen is given as,
Here,
Calculation:
Refer to table 3.5 “Properties of various aluminum alloy” value obtained from this table is,
The expression for the area of the specimen can be calculated as,
The expression for mass of the specimen can be calculated as,
Conclusions:
Therefore, the minimum weight of a
(e)
The minimum weight of a
(e)
Answer to Problem 3.54P
The minimum weight of a
Explanation of Solution
Given:
The length of the wire is
The load supported by the member is
Formula used:
The expression for area of the specimen is given as,
Here,
The expression for mass of the specimen is given as,
Here,
Calculation:
Refer to table 3.5 “Properties of various aluminum alloy” value obtained from this table is,
The expression for the area of the specimen can be calculated as,
The expression for mass of the specimen can be calculated as,
Conclusions:
Therefore, the minimum weight of a
(f)
The minimum weight of a
(f)
Answer to Problem 3.54P
The minimum weight of a
Explanation of Solution
Given:
The length of the wire is
The load supported by the member is
Formula used:
The expression for the area of the specimen is given as,
Here,
The expression for mass of the specimen is given as,
Here,
Calculation:
The expression for the area of the specimen can be calculated as,
The expression for mass of the specimen can be calculated as,
Conclusions:
Therefore, the minimum weight of a
Want to see more full solutions like this?
Chapter 3 Solutions
Pearson eText for Manufacturing Processes for Engineering Materials -- Instant Access (Pearson+)
- Q10) Body A weighs 600 lb contact with smooth surfaces at D and E. Determine the tension in the cord and the forces acting on C on member BD, also calculate the reaction at B and F. Cable 6' 3' wwwarrow_forwardHelp ارجو مساعدتي في حل هذا السؤالarrow_forwardQ3: Find the resultant of the force system.arrow_forward
- Question 1 A three-blade propeller of a diameter of 2 m has an activity factor AF of 200 and its ratio of static thrust coefficient to static torque coefficient is 10. The propeller's integrated lift coefficient is 0.3.arrow_forward(L=6847 mm, q = 5331 N/mm, M = 1408549 N.mm, and El = 8.6 x 1014 N. mm²) X A ΕΙ B L Y Marrow_forwardCalculate the maximum shear stress Tmax at the selected element within the wall (Fig. Q3) if T = 26.7 KN.m, P = 23.6 MPa, t = 2.2 mm, R = 2 m. The following choices are provided in units of MPa and rounded to three decimal places. Select one: ○ 1.2681.818 O 2. 25745.455 O 3. 17163.636 O 4. 10727.273 ○ 5.5363.636arrow_forward
- If L-719.01 mm, = 7839.63 N/m³, the normal stress σ caused by self-weight at the location of the maximum normal stress in the bar can be calculated as (Please select the correct value of σ given in Pa and rounded to three decimal places.) Select one: ○ 1. 1409.193 2. 845.516 O 3. 11273.545 ○ 4.8455.159 ○ 5.4509.418 6. 2818.386 7.5636.772arrow_forwardTo calculate the rotation at Point B, a suitable virtual structure needs to be created. Which equation in the following choices most accurately represents the functional relationship between the bending moment, Mv2 ( Units: N.mm), of the virtual structure and the spatial coordinate x (Units: mm) if the applied unit virtual moment is clockwise? Select one: O 1. Mv2 1.000 O 2. Mv2=x+1.000 O 3. Mv2=x+0.000 4. Mv2 = -x-1.000 O 5. Mv2 -1.000 6. Mv2=-x+0.000arrow_forwardThe vertical deflection at Point B can be calculated as ( The following choices are provided in units of mm and rounded to three decimal places ; the downward deflection is negative and upward deflection is positive. ) Select one: 1. 1703.065 2. -1703.065 3. -2043.679 4.1362.452 5. -1362.452 6. 2043.679arrow_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