Structural Analysis, Si Edition (mindta...6th EditionKASSIMALI, Aslam Publisher: Cengage LearningISBN: 9781337630948
Structural Analysis, Si Edition (mindta...
Solutions for Structural Analysis, Si Edition (mindtap Course List)
Browse All Chapters of This Textbook
Chapter 2 - Loads On StructuresChapter 3 - Equilibrium And Support ReactionsChapter 4 - Plane And Space TrussesChapter 5 - Beams And Frames: Shear And Bending MomentChapter 6 - Deflections Of Beams: Geometric MethodsChapter 7 - Deflections Of Trusses, Beams, And Frames: Work-energy MethodsChapter 8 - Influence LinesChapter 9 - Application Of Influence LinesChapter 10 - Analysis Of Symmetric StructuresChapter 12 - Approximate Analysis Of Rectangular Building Frames
Book Details
Master the basic principles of structural analysis using the classical approach found in Kassimali's distinctive STRUCTURAL ANALYSIS, SI Edition, 6th Edition. This edition presents concepts in a logical order, progressing from an introduction of each topic to an analysis of statically determinate beams, trusses and rigid frames, and then to the analysis of statically indeterminate structures. Practical, solved problems integrated throughout the presentation help illustrate and clarify the book's fundamental concepts, while the latest examples and timely content reflect today's most current professional standards. For further support, you can download accompanying interactive software for analyzing plane framed structures from this edition's companion website. Trust Kassimali's STRUCTURAL ANALYSIS, SI Edition, 6th Edition for the tools and knowledge you need for advanced study and professional success.
Sample Solutions for this Textbook
We offer sample solutions for Structural Analysis, Si Edition (mindtap Course List) homework problems. See examples below:
Given information: The building is a single-story building. The building is subjected to uniformly...Given information: The thickness of the reinforced concrete slab is 4 in. The area of cross-section...Given information: The structure is given in the Figure. Type of supports and reactions: Let the...Given information: The structure is given in the Figure. Length of the trolley is 5 m. Apply the...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 Figure of plane truss is shown. Calculation: Show the conditions for plane...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: Apply the sign conventions for calculating reactions, forces and moments using...Sign conversion: Apply the sign convention for calculating the equations of equilibrium as below....Chapter 5, Problem 22PChapter 5, Problem 27PChapter 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...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 29,000 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: Influence line for shear at point B: Apply a 1 kN 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: Influence line for vertical reaction at support B. Apply a 1 k unit moving load at a...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...Calculation: Apply a 1 kN unit moving load at a distance of x from left end A. Sketch the free body...Calculation: Apply a 1 k 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 the area A is...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 is...Given information: The structure is given in the Figure. The young’s modulus E and area A is...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
Structural Analysis - MindTap (12 Months)
5th Edition
ISBN: 9781285866154
EBK STRUCTURAL ANALYSIS
5th Edition
ISBN: 9780100469105
EBK STRUCTURAL ANALYSIS
5th Edition
ISBN: 8220100469107
EBK STRUCTURAL ANALYSIS
5th Edition
ISBN: 9781305142893
Structural Analysis (MindTap Course List)
5th Edition
ISBN: 9781133943891
Structural Analysis, 5th Edition
5th Edition
ISBN: 9788131520444
Structural Analysis, Si Edition
5th Edition
ISBN: 9781285051505
STRUCTURAL ANALYSIS W MINDTAP (NEW!!)
5th Edition
ISBN: 9781305361126
Structural Analysis, SI Edition
6th Edition
ISBN: 9780357030981
STRUCTURAL ANALYSIS (LL)
6th Edition
ISBN: 9780357030967
EBK STRUCTURAL ANALYSIS
6th Edition
ISBN: 9780357030974
Structural Analysis
6th Edition
ISBN: 9781337630931
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