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(a)
Interpretation:
Thematerial having highest value of density should be determined.
Concept introduction:
Density is defined as the ratio of mass per unit volume.
Where,
m is the mass of material (kg)
v is the volume of material in (m3)
The unit of density is kg/m3
(b)
Interpretation:
The material having highest value of tensile strength should be determined.
Concept introduction:
Tensile strength is defined as the ratio of force per unit area.
Where,
F is the force
A is the area
Unit of tensile strength is pascal.
(c)
Interpretation:
The material having highest value of elastic modulus should be determined.
Concept introduction:
Elastic Modulus is defined as the ratio of tensile stress to tensile strain.
Unit of elastic modulus is pascal and psi.
(d)
Interpretation:
The material having highest value of melting temperature should be determined.
Concept introduction:
Melting temperature of material is defined as the temperature at which the material changes its phase from solid to liquid phase.
Unit of melting temperature is in degree centigrade.
(e)
Interpretation:
The material having highest value of specificmodulusshould be determined.
Concept introduction:
Specific modulus is defined as the ratio of elastic modulus of material to density of material.
Unit of melting temperature is J/kg.
(f)
Interpretation:
The material having highest value of specific strength should be determined.
Concept introduction:
Specific modulus is defined as the ratio of strength of material to density of material.
Unit of melting temperature is N.m/kg
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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
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