
(a)
Interpretation:
The weight of part for the given condition is to be calculated if the part is made up of aluminum reinforced with boron fiber.
Concept introduction:
The rule of mixtures for particulate composites is:
Where
Volume fraction is defined as
Modulus of elasticity is defined as the ratio of shear stress to shear strain
Relation for modulus of elasticity is given as:

Answer to Problem 17.33P
The requiredvalue of weight of part=
Explanation of Solution
Given information:
Modulus of elasticity for titanium =
Part of 1000 pound is made
Considering modulus of elasticity parallel to fiber.
Based on given information.
Applying rule of mixing,
Calculation of volume of boron, expressed as the ratio of mass of boron to density of boron:
Mass of part =
Density of part =
Conversion of mass in gram, therefore multiplying the units by 1000 grams:
The volume of part is
Using the relation of modulus of elasticity
Using the relation of volume fraction that is the sum of sum of all volume fraction is equal to one which is given by relation,
Substituting the values in modulus of elasticity formula:
Calculation of volume fraction of aluminum:
Applying rule of mixing using the values of calculated volume fraction and density of both the components.
Calculation of weight of part using the density of part which is defined as the ratio of mass per unit volume, given by relation:
Thus, the required value of mass of part is
(b)
Interpretation:
The weight of part for polyester is to be calculated if the part is reinforced with carbon fiber.
Concept introduction:
The rule of mixtures for particulate composites:
Where
Volume fraction is defined as
Modulus of elasticity is defined as the ratio of shear stress to shear strain
Relation for modulus of elasticity is given as:

Answer to Problem 17.33P
The required value of weight of part for polyester is
Explanation of Solution
Given information:
Modulus of polyester = 650000 psi
Calculation of volume fraction of carbon and polyesters using the relation based on rule of mixing, which states that the sum of volume fraction is equal to one given by relation:
Putting the values of volume fraction of polyester in terms of volume fraction of carbon using the formula of modulus of elasticity:
Substituting the values in the formula of modulus of elasticity:
Calculation of volume fraction of polyester using the relation:
Calculation of density of part using rule of mixing and substituting the value,
Calculation of weight of part if polyester is reinforced with carbon fiber based on its relation with mass and volume.
Defining the relation as density is defined as the ratio of mass per unit volume stated as:
Substituting the value of V calculated from part (a) as
Thus, the calculated value of weight of part is
(c)
Interpretation:
The Specific Modulus fortitanium, boron and carbon is to be calculated.
Concept introduction:
Specific modulus is defined as the ratio of modulus of elasticity to density, given by relation

Answer to Problem 17.33P
The required value of specific modulus for titanium=
The required value of specific modulus for boron =
The required value of specific modulus for carbon =
Explanation of Solution
Calculation of specific modulus for titanium, using the values from part (a):
Conversion of mega pascal to
Calculation of specific modulus for titanium alloy:
Similarly calculating specific composition of boron
Modulus of elasticity of boron =
Density of boron =
Calculation of specific modulus for carbon
Thus the required values of specific modulus for titanium, boron and carbon are
Want to see more full solutions like this?
Chapter 17 Solutions
Essentials Of Materials Science And Engineering
- 1. Checksum. Assuming the following IP header lacking checksum: 01000101.00000000.11000011.00101010. 00000000.00000000.00000000.00000000. 10000000.00000000.00000000.00000000. <- checksum 01100011.11011001.00000000.00000001. 10000000.00000000.00000000.00000010 Compute its checksumarrow_forwardAssume a Space Launch System (Figure 1(a)) that is approximated as a cantilever undamped single degree of freedom (SDOF) system with a mass at its free end (Figure 1(b)). The cantilever is assumed to be massless. Assume a wind load that is approximated with a concentrated harmonic forcing function p(t) = posin(ωt) acting on the mass. The known properties of the SDOF and the applied forcing function are given below. • Mass of SDOF: m =120 kip/g • Acceleration of gravity: g = 386 in/sec2 • Bending sectional stiffness of SDOF: EI = 1015 lbf×in2 • Height of SDOF: h = 2000 inches • Amplitude of forcing function: po = 6 kip • Forcing frequency: f = 8 Hzarrow_forward13.44 The end of a cylindrical liquid cryogenic propellant tank in free space is to be protected from external (solar) radiation by placing a thin metallic shield in front of the tank. Assume the view factor Fts between the tank and the shield is unity; all surfaces are diffuse and gray, and the surroundings are at 0 K. Tank T₁ Shield, T T₁ = 100 K E1 Solar irradiation Gs ε₁ = ε₂ = 0.05 ε₁ = 0.10 Gs = 1250 W/m² E2 Find the temperature of the shield T, and the heat flux (W/m²) to the end of the tank.arrow_forward
- question 664 thank youarrow_forward5. Determine an expression for vo as a function of vs in the circuit shown below. Assume the operational amplifier is ideal (10 pts) 162 + + 212 10052} -j 100-52 Noarrow_forward13.38 Consider the attic of a home located in a hot climate. The floor of the attic is characterized by a width of L₁ = 8 m while the roof makes an angle of 0 = 30° from the horizontal direction, as shown in the schematic. The homeowner wishes to reduce the heat load to the home by adhering bright aluminum foil (ε = 0.07) onto the surfaces of the attic space. Prior to installation of the foil, the surfaces are of emissivity & = 0.90. Attic A2, 82, T2 0 = 30° A1, E1, T₁ 土 L₁ = 8 m (a) Consider installation on the bottom of the attic roof only. Determine the ratio of the radiation heat transfer after to before the installation of the foil. (b) Determine the ratio of the radiation heat transfer after to before installation if the foil is installed only on the top of the attic floor. (c) Determine the ratio of the radiation heat transfer if the foil is installed on both the roof bottom and the floor top.arrow_forward
- I would like to know the features of BranchCache, Metadata, and LPR Port Monitorarrow_forward13.1 Determine F2 and F2 for the following configura- tions using the reciprocity theorem and other basic shape factor relations. Do not use tables or charts. (a) Small sphere of area A, under a concentric hemi- sphere of area A₂ = 3A₁ A₂ A1 (a) (b) Long duct. Also, what is F₁₂? A₂ Αν (b) (c) Long inclined plates (point B is directly above the center of A₁) B 100 mm A₂ - 220 mm (c) (d) Long cylinder lying on infinite plane + A₁ Az (d) (e) Hemisphere-disk arrangement -A₂, hemisphere, diameter D A₂ A₁, disk, diameter D/2 (e) (f) Long, open channel 1 m AA₂ 2 m (f) (g) Long cylinders with A₁ = 4A₁. Also, what is F₁₂? -D₁ A1 -A₂ -D2 (e) (h) Long, square rod in a long cylinder. Also, what is F22? w=D/5 18 A₁ -A2 (h) -Darrow_forwardThe direction of the force F_11 is __________LB. The magnitude of the force F_11 is __________LB.arrow_forward
- 4. A 120 volt rms voltage source supplies 20 Amps rms to a load. The load requires 2,078 watts. What is the reactive power (Vars) and the power factor of the load. Assume the load is inductive. (15pts)arrow_forward6. Determine the rms value of the voltage cyclical waveform shown below. (15 pts) Zv N 시 ما Msec 8arrow_forward7. If the power factor of a load is unity is this also the condition for maximum power transfer? Why or why not? (10 pts)arrow_forward
- MATLAB: An Introduction with ApplicationsEngineeringISBN:9781119256830Author:Amos GilatPublisher:John Wiley & Sons IncEssentials Of Materials Science And EngineeringEngineeringISBN:9781337385497Author:WRIGHT, Wendelin J.Publisher:Cengage,Industrial Motor ControlEngineeringISBN:9781133691808Author:Stephen HermanPublisher:Cengage Learning
- Basics Of Engineering EconomyEngineeringISBN:9780073376356Author:Leland Blank, Anthony TarquinPublisher:MCGRAW-HILL HIGHER EDUCATIONStructural Steel Design (6th Edition)EngineeringISBN:9780134589657Author:Jack C. McCormac, Stephen F. CsernakPublisher:PEARSONFundamentals of Materials Science and Engineering...EngineeringISBN:9781119175483Author:William D. Callister Jr., David G. RethwischPublisher:WILEY





