| a. a high elastic modulus. | ||
| b. a high melting temperature. | ||
| c. a high yield strength. | ||
| d. a long fatigue life. |
| a. We do not expect creep deformation to occur. | ||
| b. Fast fracture should occur before creep deformation begins. | ||
| c. We do expect creep deformation to occur. | ||
| d. We do not have enough information to predict creep deformation. |
| a. plastic yielding | ||
| b. creep permanent strain. | ||
| c. fast fracture. | ||
| d. non-protective oxide films. |
| a. percent elongation. | ||
| b. hardness. | ||
| c. elastic modulus. | ||
| d. ultimate tensile strength. |
| a. elastic modulus. | ||
| b. Poisson's ratio. | ||
| c. yield stress. | ||
| d. tensile strength. |
| a. shear modulus. | ||
| b. yield stress. | ||
| c. percent elongation. | ||
| d. creep rate. |
| a. hardness. | ||
| b. yield strength. | ||
| c. creep resistance. | ||
| d. toughness. |
| a. in jet engines. | ||
| b. in automobile engines. | ||
| c. with aircraft wings. | ||
| d. with plastics at low temperatures. |
| a. at low temperatures. | ||
| b. at high temperatures. | ||
| c. when vibration is present. | ||
| d. when materials are in an oxygen-rich environment. |
| a. impact testing. | ||
| b. fatigue testing. | ||
| c. creep testing. | ||
| d. tensile testing. |
| a. is crack propagation at the speed of sound. | ||
| b. is always preceded by plastic yielding. | ||
| c. occurs only at low temperatures. | ||
| d. is observed in ceramics, but never in metals. |
| a. may be either less than or greater than the yield stress. | ||
| b. is always less than the yield stress. | ||
| c. is always greater than the yield stress. | ||
| d. is not usually measured in the tensile test. |
| a. is linear stress-strain behavior. | ||
| b. is parabolic stress-strain behavior. | ||
| c. obeys the Arrhenius law. | ||
| d. results in permanent shape change. |
| a. can identify polymers. | ||
| b. are completely non-destructive. | ||
| c. cannot be made on ceramics. | ||
| d. often follow heat treatment of metals. |
| a. yield stress. | ||
| b. creep rate. | ||
| c. fatigue life. | ||
| d. stiffness. |
| a. brittle fracture. | ||
| b. protective oxide films. | ||
| c. non-protective oxide films. | ||
| d. stainless steels. |
| a. have low melting points. | ||
| b. have a high percent elongation. | ||
| c. have a low yield stress. | ||
| d. have low percent area reduction values. |
| a. is always corrosive. | ||
| b. can sometimes be beneficial. | ||
| c. doesn't occur with many metals. | ||
| d. can be avoided by operating at high temperatures. |
| a. only occurs at elevated temperatures. | ||
| b. is irreversible shape change. | ||
| c. can sometimes be reversible shape change. | ||
| d. always fractures the part. |
| a. fast fracture. | ||
| b. plastic yielding. | ||
| c. excessive creep strain. | ||
| d. non-protective oxide formation. |
| a. stiffness. | ||
| b. hardness. | ||
| c. toughness. | ||
| d. fatigue life. |
| a. in a tensile test. | ||
| b. in a fatigue test. | ||
| c. in a creep test. | ||
| d. in a hardness machine. |
| a. using materials with parabolic oxide growth rates. | ||
| b. utilizing a sacrificial cathode. | ||
| c. utilizing a sacrificial anode. | ||
| d. using materials with linear oxide growth rates. |
| a. final hardness. | ||
| b. cycles to failure. | ||
| c. impact strength. | ||
| d. temperature variations. |
| a. annealing. | ||
| b. straining. | ||
| c. melting. | ||
| d. strengthening. |
| a. always results in a decrease in volume. | ||
| b. occurs with constant volume. | ||
| c. always results in an increase in volume. | ||
| d. can either increase or decrease the volume. |
| a. wet corrosion rates. | ||
| b. protective oxide films. | ||
| c. cathode and anode identification. | ||
| d. corrosion electrical currents. |
| a. meters squared (or feet squared). | ||
| b. dimensionless. | ||
| c. newtons/meters squared (or pounds per square inch). | ||
| d. newtons (or pounds). |
| a. pascals. | ||
| b. seconds. | ||
| c. meters squared. | ||
| d. dimensionless. |
| a. pascals. | ||
| b. pascals times square root of meters. | ||
| c. percent per square meter. | ||
| d. dimensionless. |
| a. stress versus cycles. | ||
| b. stress versus strain. | ||
| c. strain versus time. | ||
| d. mass gain versus time. |
| a. minimize the cathode area. | ||
| b. minimize the anode area. | ||
| c. make the anode and cathode areas as nearly equal as possible. | ||
| d. ignore areas as corrosion rate is not strongly dependent on area. |
| a. Residual tensile stresses in the surface | ||
| b. Sharp corners in the sample geometry | ||
| c. Rough surface texture | ||
| d. Residual compression stresses in the surface |
| a. decrease creep strain rate. | ||
| b. increase stiffness. | ||
| c. increase impact energy absorption. | ||
| d. lengthen fatigue life. |
| a. plastic deformation followed by elastic deformation. | ||
| b. elastic deformation followed by plastic deformation. | ||
| c. elastic deformation only. | ||
| d. plastic deformation only. |
| a. necking down of polymer materials. | ||
| b. a property of brittle materials. | ||
| c. an increase in yield stress. | ||
| d. an increase in stiffness. |
| a. show creep deformation at relatively low temperatures. | ||
| b. oxidize rapidly. | ||
| c. cannot be alloyed to be heat treatable. | ||
| d. have low thermal conductivity. |
| a. often interact with atmospheres. | ||
| b. can be difficult to shape. | ||
| c. tend to deform by creep. | ||
| d. lose their ductility at low temperatures. |
| a. they are relatively expensive. | ||
| b. they are chemically reactive. | ||
| c. they have high strength to weight ratios. | ||
| d. they cannot be heat treated. |
| a. they are typically very hard. | ||
| b. they can easily be formed into complex shapes. | ||
| c. they have high percent elongation. | ||
| d. they have high densities. |
| a. they usually have high melting temperatures. | ||
| b. they are hard and scratch resistant. | ||
| c. they have low elastic modulus values. | ||
| d. they are usually chemically inert. |
| a. show a volume change like melting ice. | ||
| b. change color. | ||
| c. change smoothly between rigid solid and viscous liquid. | ||
| d. permanently set up into rigid solids. |
| a. brittle and electrically insulating. | ||
| b. tough and hard. | ||
| c. flexible and high melting. | ||
| d. low density and soft. |
| a. result in ions packing close together. | ||
| b. are consistent with the high electrical conductivity of metals. | ||
| c. are easily broken during plastic deformation. | ||
| d. result in lower density solids. |
| a. stiffens it. | ||
| b. causes it to flow more freely. | ||
| c. increases the glass transition temperature. | ||
| d. improves oxidation resistance. |
| a. a hard, strong phase forms. | ||
| b. the steel softens slightly. | ||
| c. oxide formation is reduced. | ||
| d. the operating temperature of the final steel product is increased. |
| a. polycrystalline reinforced. | ||
| b. particle remelted. | ||
| c. polymer resins. | ||
| d. plastic remolded. |
| a. are always quench hardened. | ||
| b. are the construction I-beam steels. | ||
| c. have particularly good corrosion resistance. | ||
| d. have relatively large amounts of other alloying elements. |
| a. have low densities. | ||
| b. have high melting temperatures. | ||
| c. exhibit low electrical conductivity. | ||
| d. also exhibit high electrical conductivity. |
| a. isotropic behavior (same in all directions). | ||
| b. light weight. | ||
| c. high melting temperature. | ||
| d. low cost. |
| a. polymers. | ||
| b. ceramics. | ||
| c. composite materials. | ||
| d. metals. |
| a. covalent bonds readily stretch. | ||
| b. long chain molecules can uncoil and recoil. | ||
| c. polymer molecules easily slide over one another. | ||
| d. ionic bonds are easily broken. |
| a. the light weight of some metals. | ||
| b. the high electrical and thermal conductivities of most metals. | ||
| c. the tendency of metals to corrode. | ||
| d. the brittleness of some metals. |
| a. results in a hard structure. | ||
| b. results in a soft structure. | ||
| c. causes a phase change within the alloy. | ||
| d. is required to clean the alloy surface. |
| a. are rubbery materials. | ||
| b. are permanent once cured. | ||
| c. are usable to higher temperatures than other polymers types. | ||
| d. can be repeatedly softened and stiffened. |
| a. are recyclable. | ||
| b. are frequently rubber-like. | ||
| c. include the hard, rigid Bakelite® and melamine plastics. | ||
| d. are usually clear or translucent. |
| a. composite materials. | ||
| b. metals. | ||
| c. polymers. | ||
| d. ceramics. |
| a. have low thermal expansion coefficients. | ||
| b. have high thermal expansion coefficients. | ||
| c. have high softening temperatures. | ||
| d. have low densities. |
| a. Nickel-based super alloy turbine blade | ||
| b. Wood | ||
| c. Reinforced concrete | ||
| d. Graphite reinforced tennis racket frame. |
| a. tungsten carbide tool inserts. | ||
| b. porcelain plates. | ||
| c. silicon carbide abrasives. | ||
| d. diamonds. |
| a. is considered to be ductile. | ||
| b. is considered to be brittle. | ||
| c. is most likely low density. | ||
| d. is most likely of a low melting temperature. |
| a. endurance limit. | ||
| b. hardness number. | ||
| c. melting or softening temperature in kelvin. | ||
| d. elastic stiffness. |
| a. its elastic stiffness increases. | ||
| b. its melting temperature decreases. | ||
| c. its yield stress increases. | ||
| d. its volume increases. |
| a. creep. | ||
| b. plastic yielding. | ||
| c. fast fracture. | ||
| d. oxidation. |
| a. when corrosion is occurring. | ||
| b. at low temperatures. | ||
| c. at high temperatures. | ||
| d. when vibration is present. |
| a. the elastic modulus is very low. | ||
| b. the percent elongation is very high. | ||
| c. the tensile strength is much higher than the yield stress. | ||
| d. the tensile strength is much lower than the yield stress. |
| a. metals. | ||
| b. plastics. | ||
| c. ceramics. | ||
| d. composite materials. |
| a. rupture modulus. | ||
| b. elastic modulus. | ||
| c. hardness number. | ||
| d. percent elongation. |
| a. we should select the material with the highest elastic modulus. | ||
| b. we should select the material with the highest melting temperature. | ||
| c. we cannot generalize without knowing the geometry of the part. | ||
| d. we should select the material with the highest yield strength. |
| a. plastic. | ||
| b. metal. | ||
| c. ceramic. | ||
| d. composite material. |
| a. creep. | ||
| b. impact. | ||
| c. fatigue. | ||
| d. tension. |
| a. metals. | ||
| b. polymers. | ||
| c. composite materials. | ||
| d. ceramics. |
| a. fatigue failure. | ||
| b. creep failure. | ||
| c. stress corrosion. | ||
| d. elastic recovery. |
| a. linear. | ||
| b. non-linear. | ||
| c. restricted to approximately 0.2% strain. | ||
| d. showing a higher elastic modulus than for most metals. |
| a. kg/m³. | ||
| b. kilograms. | ||
| c. m/s². | ||
| d. dimensionless. |
| a. with fine (small) grains. | ||
| b. with coarse (large) grains. | ||
| c. with high yield strengths. | ||
| d. with low melting temperatures. |
| a. critical stress intensity factor. | ||
| b. hardness number. | ||
| c. density. | ||
| d. melting temperature. |
| a. the cathode areas should be small. | ||
| b. the anode areas should be small. | ||
| c. metals should be widely separated in the electrochemical series. | ||
| d. surfaces should be rough rather than smooth. |
| a. Non-protective oxide film | ||
| b. Contact with an aqueous solution | ||
| c. Electrical contact between anode and cathode | ||
| d. Two dissimilar metals |
| a. Using polished surfaces | ||
| b. Strain hardening | ||
| c. Introducing compressive surface residual stresses | ||
| d. Reducing geometries of sharp corners |
| a. more dense metal. | ||
| b. the standard electrode. | ||
| c. the cathode. | ||
| d. the anode. |
| a. creep. | ||
| b. fast fracture. | ||
| c. excessive plastic deformation. | ||
| d. necking down to concentrate stress. |
| a. the iron is the sacrificial anode. | ||
| b. the zinc is the sacrificial anode. | ||
| c. either iron or zinc can be the anode. | ||
| d. both the iron and zinc corrode simultaneously. |
| a. high percent elongation. | ||
| b. low yield strength. | ||
| c. low melting temperatures. | ||
| d. low density. |
| a. though stronger, final parts are also more brittle. | ||
| b. long rod and tube shapes cannot be formed. | ||
| c. it cannot be used with materials at high temperatures. | ||
| d. porous, low density products may result. |
| a. parts are generally limited to be small in size. | ||
| b. porous, low-density products may result. | ||
| c. preferred textures may be in the final products. | ||
| d. only low-temperature materials can be formed this way. |
| a. chemically reacting materials cannot be cast. | ||
| b. extensive post machining may be required. | ||
| c. some materials deteriorate before they melt. | ||
| d. porous, low-density products may result. |
| a. directional solidification. | ||
| b. preferred orientation stamping. | ||
| c. oxyacetylene torch cutting. | ||
| d. lost wax casting. |
| a. the porous product can be utilized for specialized applications. | ||
| b. dissimilar materials can be joined together. | ||
| c. metals can be strengthened while being shaped. | ||
| d. intricate shapes can be formed in a single step. |
| a. dissimilar materials can be joined together. | ||
| b. intricate shapes can be formed in a single step. | ||
| c. the porous product can be utilized for specialized applications. | ||
| d. metals can be strengthened while being shaped. |
| a. refractory (very high melting) materials can be shaped. | ||
| b. metals can be strengthened while being shaped. | ||
| c. dissimilar materials can be joined together. | ||
| d. preferred texture can be imparted to the final part. |
| a. dissimilar materials can be joined together. | ||
| b. it can be used to cut as well as join metals. | ||
| c. acetylene gas is explosive. | ||
| d. it can be automated for use with industrial robots. |
| a. very fine powders can be explosive. | ||
| b. large electrical currents pass through the parts. | ||
| c. temperatures involved are higher than the melting temperatures. | ||
| d. corrosive chemicals are required. |
| a. casting. | ||
| b. sintering. | ||
| c. compressive mechanical forming. | ||
| d. TIG welding. |
| a. MIG welding. | ||
| b. TIG welding. | ||
| c. oxyacetylene welding. | ||
| d. shielded metal arc welding. |
| a. displaced grain boundaries. | ||
| b. linear geometric defects. | ||
| c. impurity concentrations. | ||
| d. responsible for elastic deformation. |
| a. refers to the weld filler metal. | ||
| b. is stronger than the surrounding metal. | ||
| c. is severely work hardened. | ||
| d. may no longer be corrosion resistant. |
| a. casting. | ||
| b. extrusion. | ||
| c. TIG welding. | ||
| d. hot rolling. |
| a. its yield stress increases. | ||
| b. its fracture toughness is decreased. | ||
| c. recrystallization grows new grains within the metal. | ||
| d. its dislocation density is increased. |
| a. It frequently is used to cut as well as join. | ||
| b. The tungsten electrode is not consumed during the welding. | ||
| c. TIG requires greater operator skill than other welding processes. | ||
| d. It is usually the first choice for joining stainless steels. |