Structural Analysis (MindTap Course List) - 5th Edition - by Aslam Kassimali - ISBN 9781133943891

Structural Analysis (MindTap Course Lis...
5th Edition
Aslam Kassimali
Publisher: Cengage Learning
ISBN: 9781133943891

Solutions for Structural Analysis (MindTap Course List)

Book Details

The 5th edition of the classic STRUCTURAL ANALYSIS by Aslam Kassamali teaches students the basic principles of structural analysis using the classical approach. The chapters are presented in a logical order, moving from an introduction of the topic to an analysis of statically determinate beams, trusses and rigid frames, to the analysis of statistically indeterminate structures. The text includes solved problems to help illustrate the fundamental concepts. Access to interactive software for analyzing plane framed structures is available for download via the text's companion website.

Sample Solutions for this Textbook

We offer sample solutions for Structural Analysis (MindTap Course List) homework problems. See examples below:

Given information: Apply the sign conventions for calculating reactions, forces and moments using...Given information: Apply the sign conventions for calculating reactions, forces and moments using...Given information: Apply the sign conventions for calculating reactions, forces and moments using...Given information: Apply the sign conventions for calculating reactions, forces and moments using...Given information: The point load acting at the distance of 5 m from the left support (P1) is 60 kN....Chapter 5, Problem 22PChapter 5, Problem 28PWrite the condition for static instability, determinacy and indeterminacy of plane frames as...Write the condition for static instability, determinacy and indeterminacy of plane frames as...Write the condition for static instability, determinacy and indeterminacy of plane frames as...Write the condition for static instability, determinacy and indeterminacy of plane frames as...Write the condition for static instability, determinacy and indeterminacy of plane frames as...Calculation: Consider the flexural rigidity EI of the beam is constant. Draw the free body diagram...Calculation: Draw the free body diagram of the beam as in Figure (1). Refer Figure (1), Find the...Calculation: Consider flexural rigidity EI of the beam is constant. Draw the free body diagram of...Given information: The Young’s modulus (E) is 29,000 ksi. The moment of inertia (I) is 4,000 in.4....Given information: The Young’s modulus (E) is 29,000 ksi. The moment of inertia (I) is 6,000 in.4....Given information: The Young’s modulus (E) is 30,000 ksi. The moment of inertia of the section AB is...Given information: The Young’s modulus (E) is 30,000 ksi. The moment of inertia of the section AB is...Given information: The truss is given in the Figure. The value of E is 10,000 ksi and the value of A...Given information: The truss is given in the Figure. The value of E is 70 GPa and the value of A is...Given information: The truss is given in the Figure. The value of E is 200 GPa and the value of A is...Given information: The truss is given in the Figure. The value of E is 200 GPa. Procedure to find...Given information: The beam is given in the Figure. Value of E is 30,000 ksi, I is 4,000 in.4 for...Given information: The frame is given in the Figure. The value of E is 200 GPa and I is 350×106 mm4....Given information: The beam is given in the Figure. Value of E is 30,000 ksi, I is 4,000 in.4 for...Calculation: Apply a 1 k unit moving load at a distance of x from left end A. Sketch the free body...Calculation: Equation of influence line ordinate of support B: Apply a 1 k unit moving load at a...Equation of influence line ordinate of support B: Apply a 1 k unit moving load at a distance of x...Calculation: Influence line for moment at support A. Apply a 1 kN unit moving load at a distance of...Calculation: Apply a 1 kN unit moving load at a distance of x from left end D. Sketch the free body...Calculation: Find the support reactions. Apply 1 k moving load from A to G in the bottom chord...Calculation: Find the support reactions. Apply 1 k moving load from E to G in the top chord member....Given Information: The concentrated live load (P) is 75 kN. Calculation: Apply a 1 kN unit moving...Given Information: The concentrated live load (P) is 150 kN. The uniformly distributed live load...Calculation: Apply a 1 kN unit moving load at a distance of x from left end A. Sketch the free body...Given information: The structure is given in the Figure. The Young’s modulus E and area A are...Given information: The structure is given in the Figure. The young’s modulus E and area A is...Given information: The structure is given in the Figure. The young’s modulus E and area A are...Given information: The structure is given in the Figure. The young’s modulus E and area A are...Given information: The uniformly distributed load acting along the girder DEF (w) is 30 kN/m. The...Given information: The axial force acting at point I (HI) is 20 kN. The axial force acting at point...Given information: The axial force acting at point M (HM) is 7.5 k. The axial force acting at point...Given information: Apply the sign conventions for calculating reactions, forces, and moments using...Given information: The structure is given in the Figure. Apply the sign conventions for calculating...Given information: The structure is given in the Figure. Apply the sign conventions for calculating...Given information: The structure is given in the Figure. Apply the sign conventions for calculating...Given information: The structure is given in the Figure. Apply the sign conventions for calculating...Given information: The structure is given in the Figure. Apply the sign conventions for calculating...Given information: The settlement at A (ΔA) is 10 mm=0.01 m. The settlement at C (ΔC) is 65 mm=0.065...Fixed end moment: Formula to calculate the fixed moment for point load with equal length are PL8....Fixed end moment: Formula to calculate the fixed moment for point load with equal length are PL8....Fixed end moment: Formula to calculate the fixed moment for UDL is WL212. Calculation: Consider the...Calculation: Consider the elastic modulus E of the frame is constant. Show the free body diagram of...Fixed end moment: Formula to calculate the relative stiffness for fixed support IL and for roller...Fixed end moment: Formula to calculate the relative stiffness for fixed support IL and for roller...Fixed end moment: Formula to calculate the relative stiffness for fixed support IL and for roller...Fixed end moment: Formula to calculate the relative stiffness for fixed support IL and for roller...Given information: A=[12−815−87101510−5] B=[2−11−146163] Calculation: Find the matrix 3B: Substitute...Given information: A=[420−323−400−42−1−30−15] Calculation: Write the given matrix in augmented...Given information: The structure is given in the Figure. Apply the sign conventions for calculating...Given information: The structure is given in the Figure. The settlement of support A is 10 mm,...

More Editions of This Book

Corresponding editions of this textbook are also available below:

Structural Analysis
4th Edition
ISBN: 9780495295655
EBK STRUCTURAL ANALYSIS
5th Edition
ISBN: 9780100469105
Structural Analysis, 5th Edition
5th Edition
ISBN: 9788131520444

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