GMas xP Acce x Hat xHat × |Md: × 45c × Rep × Cha × |V. Try × ULT ×© Sol x New xMda x |session.masteringengineering.com/myct/itemView?assignmentProblemID=18323525&attemptNo=1&offset=prevssignment 1D (CHAPTER 5) - Attempt 1Problem 5.58Consider the hatch door in (Figure 1).FigureP2 m79°FPartly cloudy2 mB1 of 1Q SearchPart ADetermine the force in the cable as a function of 0, needed to support the 100-kg hatch door.Express your answer in terms of 8.ΕΠΙ ΑΣΦ$1?vecδE77ᎾKλμV元PTXWWAΣФΨ ΩhEP= 981 cos 0SubmiPrevious Answers Request AnswerX Incorrect; Try Again; 9 attempts remainingDB25N

The problem is asking us to find the force in the cable that is needed to support a 100-kg hatch…

Answered: G Mas x P Acce x Hat x Hat × | Md: ×…

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

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Produce a 3D solid model of the Guard casing and test boss using solid works, send the file so I can download it. Email: lukecass3456@gmail.com
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8. What are the main stages of the FEM? 9. Make a sketch of a linear triangular finite element. Point the nodes and write the approximating polynomial. 10. Describe with one sentence what the shape functions in FEM are. 11. Special case of which method is the method of Galerkin? 12. What are the three main parts of a FEM program? 13. How can be increased the accuracy of the derivatives for linear finite elements in FEM postprocessor? 14. Specify three methods for force computation in FEM postprocessor.
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INSTRUCTIONS: Solve the following problem by manually applying the finite element method, following these steps: Pre-processing: Geometry identification. Material properties identification. Load identification. Boundary condition identification. Development of the connectivity matrix for nodes and elements. Processing: Calculation of local stiffness matrices. Assembly of the global stiffness matrix. Assembly of the global force matrix (if required). Application of boundary conditions. Resolution of the system of equations. Derivation of the complete displacement vector (u). Post-processing: Reaction forces calculation. Stress analysis. Problem Statement: the truss nodes and elements (in parentheses) are already numbered. The areas (are in cm^2 ) are underlined. members are made of structural steel, modulus of elasticity is (E) of 20×10^6 N/cm^2 . the lengths are given in cm.
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