Material selection chart10000Strength - DensityCeramics| SigNaTi alloysMetalsComposites.Al203SteelsSicNi alloysAl alloysCFRPMetals and polymers: yield strengthCeramics and glasses: MOREl astomers:tensile tear strengthComposites: tensile failureTungstenalloys1000Mg alloysPolymers andelastomersTungstencarbideGFRPPEEKPETPA-Copperalloys100PMMANaturalWoodto grainmaterials10Rigid polymerfoamsZinc alloysLead alloysFoamsConcreteButylSiliconeGuide lines forminimum massdesignWood rubber1 to grainelastomersCork0.1Flexible pofymerloámsMFA, 040.010.010.1110Density, p (Mg/m3)Figure 1. Strength vs Density chartStrength, of (MPa) (b)design guideline.Using the material selection chart provided (Figure 1) and appropriate(i)Select suitable materials for the skateboard deck as a panel under thefollowing conditions: (1) minimum strength is 100 MPa, (2) a high strength perunit mass and (3) the design guideline passing through centre of the woodbubble. Show your design constraint lines on the graph provided and list theselected materials.

(1) We have to select the materials for the skateboard deck of minimum strength is 100 MPa.

Material selection chart 10000 Ceramics Strength - Density SigN4 Ti alloys Metals Composites. | A0 Steels Ni alloys Sic Al alloys W CFRP Metals and polymers: yield strength Ceramics and glasses: MOR El astomers:tensile tear strength Composites: tensile failure Tungsten alloys 1000 Polymers and elastomers Mg alloys, Tungsten carbide GFRP PEEK P PET PMMA Copper alloys 100 Wood to grain Natural materials 10 Rigid polymer foams Zinc alloys Lead alloys Foams Concrete Butyl Silicone Wood rubber 1 to grain Guide lines for minimum mass design elastomers Cork 0.1 Flexible pofymer loams MFA, O4 0.01 0.01 0.1 1 10 Density, p (Mg/m3) Figure 1. Strength vs Density chart Strength, of (MPa)

Material selection chart 10000 Ceramics Strength - Density SigN4 Ti alloys Metals Composites. | A0 Steels Ni alloys Sic Al alloys W CFRP Metals and polymers: yield strength Ceramics and glasses: MOR El astomers:tensile tear strength Composites: tensile failure Tungsten alloys 1000 Polymers and elastomers Mg alloys, Tungsten carbide GFRP PEEK P PET PMMA Copper alloys 100 Wood to grain Natural materials 10 Rigid polymer foams Zinc alloys Lead alloys Foams Concrete Butyl Silicone Wood rubber 1 to grain Guide lines for minimum mass design elastomers Cork 0.1 Flexible pofymer loams MFA, O4 0.01 0.01 0.1 1 10 Density, p (Mg/m3) Figure 1. Strength vs Density chart Strength, of (MPa)

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

Problem You are tasked with analyzing the frame of a bubble fuselage. The frame is 3D printed using PLA material and must be capable of supporting a 22.05 lb load placed within the cabin space, with the direction of the load indicating the direction of deformation. You will need to perform a series of calculations and analyses to ensure that the design meets strength and safety requirements. Data: Frame Dimensions: A blueprint is provided specifying the dimensions and geometry of the bubble fuselage frame. The thickness of the frame its 0.5 inch. Material: The frame will be 3D printed in PLA material. The material properties of PLA are as follows: Young's Modulus (E): 595669.99 Psi. Yield Strength (σy): 9094.01119 Psi. Density (ρ): 10.04515912 lb/in³ Load: A 22.05 lb load will be applied within the cabin space, with the load direction indicating the direction of deformation Tasks to Perform:( Remmember present the solution process with equations, procedure and results; use…
Problem You are tasked with analyzing the frame of a bubble fuselage. The frame is 3D printed using PLA material and must be capable of supporting a 22.05 lb load placed within the cabin space, with the direction of the load indicating the direction of deformation. You will need to perform a series of calculations and analyses to ensure that the design meets strength and safety requirements. Data: Frame Dimensions: A blueprint is provided specifying the dimensions and geometry of the bubble fuselage frame. The thickness of the frame its 0.5 inch. Material: The frame will be 3D printed in PLA material. The material properties of PLA are as follows: Young's Modulus (E): 595669.99 Psi. Yield Strength (σy): 9094.01119 Psi. Density (ρ): 10.04515912 lb/in³ Load: A 22.05 lb load will be applied within the cabin space, with the load direction indicating the direction of deformation Tasks to Perform:( Remmember present the solution process with equations, procedure and results; use…
Problem You are tasked with analyzing the frame of a bubble fuselage. The frame is 3D printed using PLA material and must be capable of supporting a 22.05 lb load placed within the cabin space, with the direction of the load indicating the direction of deformation. You will need to perform a series of calculations and analyses to ensure that the design meets strength and safety requirements. Data: Frame Dimensions: A blueprint is provided specifying the dimensions and geometry of the bubble fuselage frame. The thickness of the frame its 0.5 inch. Material: The frame will be 3D printed in PLA material. The material properties of PLA are as follows: Young's Modulus (E): 595669.99 Psi. Yield Strength (σy): 9094.01119 Psi. Density (ρ): 10.04515912 lb/in³ Load: A 22.05 lb load will be applied within the cabin space, with the load direction indicating the direction of deformation Tasks to Perform:( Remmember present the solution process with equations, procedure and results; use…
In your summer internship, you are tasked with measuring the ultimate tensile strength of a material to determine if it meets your company’s (Superior Super Ships Inc) specification. Your boss is worried that the new low-cost supplier, Shoddy Alloys Inc, may not be reliable but it is the only way to source on-time the SS304 needed to make finishings for Jeff Bezos’ new yacht, the Black Pearl. You collect several load versus displacement curves, as illustrated below. The initial diameter of the round gauge section is 0.25 in. You also collect the instantaneous diameter of the specimen during the test using a laser. Using the provided data, calculate what is the ultimate tensile strength measured in this test?
Imagine you are a Mechanical Materials Engineer working at Mazoon Electricals Company. You are assigned to select suitable material for the body of a three-pin electrical plug. Select a suitable material based on the design specification and selection criteria.
Write down a proper material for each structures given below. A pipe for water Material: Reason: exchange The nose section of an Material: aircraft fuselage Reason: The spar of an aircraft Material: wing Reason: Turbine blades of a Material: turbojet engine Reason: The skin of an aircraft Material: fuselage Reason: The structure of interior Material: furniture in aircraft cabins Reason: Material: The gearbox of a helicopter Reason: The front tips of a space Material: shuttle surface Reason:
Project 4: Design engineers in many situations must justify their selection of beams and pin-ended columns used in various machines. Your role in a mechanical design company that manufactures gearbox and gearbox mounting platform is to analyses the rolled steel beams and colunus under study. Your manager asked you to properly select one rolled steel beam and one rolled steel column for the design and to provide your justification of this selection, if the following design requirements are given: Beams and columns are made of ASTM-A709IGrade 345 - Factor of Safety (FS) is 1.4 Buckling Euler conditions must be met. Beams are subjected to 50 kN axial force. Beam (A) has radius of 10 mm. - Beam (B) has radius of 5 mm. - Column (A) is subjected to 15 kN axial force. Column (A) has length of 1.5 m and radius of 10 mm. Column (B) is subjected to 15 kN axial force. Column (B) has length of 1.5 m and radius of 13 mm. Note: Column critical load must be determined (based on Euler theory…
Statics of Rigid Bodies (S1) Note: I will report you if you answer this post multiple times so please follow it.Thank you for understanding, Tutor! Content Covered: - Analysis of Structures Direction: Solve the problem below by giving the complete solution. In return, I will give you a good and high rating. Thank you so much! Note: Be careful with the calculations in the problem. Kindly double check the solution and answer if there is a deficiency. And also, box the final answer. Thank you so much!
You work for an off-shore wind turbine manufacturer and have been asked to review data from the support structure development team. The cost of the high strength steel currently used in the support structure has increased significantly in the last 12 months so the development team have manufactured some components to an identical design using a cheaper grade of structural steel. Company policy states that the critical tensile stress must be 30% more than the expected maximum in service stress of 420MPa. Given the information below, what is critical tensile stress of the cheaper grade of structural steel and would you recommend its use in the wind turbine support structure? Alternate Steel Analysis Report: • Detected maximum internal flaw size = 1.0 μm, • Specific surface energy 1.3 J/m2, • Youngs Modulus = 210GPa Select one or more: a. 18.6 MPa b. No, would not recommend DC. 417 MPa Od. 590 MPa 0 e. Yes, would recommend Of. 13.2 MPa
INTAKE TUT Air Inlet to search COMPRESSION Combustion Chambers COMBUSTION Turbine EXHAUST
You work for an off-shore wind turbine manufacturer and have been asked to review data from the support structure development team. The cost of the high strength steel currently used in the support structure has increased significantly in the last 12 months so the development team have manufactured some components to an identical design using a cheaper grade of structural steel. Company policy states that the critical tensile stress must be 30% more than the expected maximum in service stress of 420MPa. Given the information below, what is critical tensile stress of the cheaper grade of structural steel and would you recommend its use in the wind turbine support structure? Alternate Steel Analysis Report: • Detected maximum internal flaw size = 1.0 μm, ● Specific surface energy 1.3 J/m2, ● Youngs Modulus = 210GPa Select one or more: a.590 MPa b.Yes, would recommend c.417 MPa d.13.2 MPa e.No, would not recommend f.18.6 MPa
Show the typical Stress versus Strain curve for the following materials, and define the materials properties "The stress-strain curve can be used to read off the structural load ability of materials. For many materials, including metals, their loading bearing capability is one of the most important material properties". by reference to the diagram: a) Hammer head is made from hardened tool steel b) Smelter is made from refractory ceramic c) Cable is made from pure copper d) Box is made from polypropylene