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Timothy A. Philpot - Mechanics of materials _ an integrated learning system-John Wiley (2017)

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Biaxial stress, 566–568, 587, 590–591,

656, 657, 659, 662

Boundary conditions

for beams, 396, 411, 424, 451

for columns, 671, 672, 680–682, 691

Brittle materials, 24, 52–54, 133, 141, 621,

662–663

maximum-normal-stress theory of

failure, 662

Mohr’s Failure Criterion, 662–663

Buckling

defined, 141, 667

equations, 831

Built-up beams, shear in, 346–352

Bulk modulus, 564

C

Cantilever beam

deflection formulas, 823

Cantilever beam, defined, 195

Castigliano’s First Theorem, 774

Castigliano’s Second Theorem, 774–787

applied to beams, 781–787

applied to trusses, 776–780

development of, 774–776

Center of curvature, defined, 239–240

Centric loading

combined with bending, 282–289

combined with bending and torsion,

634–652

combined with torsion, 616–619

defined, 23

stresses due to, 2–7

Centroids of areas, 790–794

Channel sections (C-shapes), 255, 256,

813–814

Circular hole, stress distribution near,

130–133

Circular shafts

deformations in, 137–138, 142–143

elastic torsion formula for, 139

moment of inertia, 260, 338–339, 636,

640, 644, 648

normal stresses in, 139–141

polar moment of inertia, 139

section modulus, 260

shear stresses in, 139–141

statically indeterminate, 166–181

strains in, 137–138

stress-concentration factors, 183–185

transverse shear stress in, 338–339

Circumferential stress (hoop stress), 308,

588–591, 598–605, 607, 612–614

Clapeyron’s theorem, 659

Code calibration, 78

Coefficient of thermal expansion, 41

of selected materials, table, 825–826

Column(s)

centric loading of, 670–688

critical load for, 672–673, 683–685

defined, 667

derivation of, 671–672, 690–695

eccentricity ratio for, 694–695

eccentric loading, 690–695, 707–713

effective length, 683–688

effective length factors, 684–685

effect of end conditions on, 680–688

empirical formulas for, 696–704

Euler’s formula, 672–673

intermediate, 675, 697–699

local instability, 699

long, 675, 697–699

short, 675, 697, 698

slenderness ratio, 673, 675, 685

Column-buckling model, 668, 831

Column formulas

AISC, 697–698

Aluminum Association, 698–699

Euler, 672–673

interaction, 708

NDS, 699

parabolic, 715

secant, 694

structural steel, 697–698

wood, 699

Combined loadings

axial and torsional, 616–619

centric, flexural, and torsional, 484,

634–652

centric and flexural, 282–289

Compatibility equation

for axial members, 103, 106, 109,

122, 124

for flexural members, 462

for torsion members, 167, 168, 170,

173, 178

Composite beams, 270

Compression, defined, 2

Compression stress, 141, 241, 282,

693–694, 697, 707

Compressive stress, 623, 707

Concentrated load, 195

Concept of stress, 2–3, 7–8, 480–481

Conservation of energy

applied to axial deformation, 718

applied to impact load, 729

applied to torsional deformation, 722

defined, 715, 717, 746

Constitutive relationships, 103

Contact pressure, 610, 611

Continuity conditions, 396–398, 451

Continuous beam, defined, 446–447

Coulomb’s theory, 657

Critical buckling load, 670, 672–673, 675

Critical buckling stress, 673–675

Cross section, defined, 2

Curvature, 240

Curvature, radius of, 239

Curved bars, 306–315

Cylinders, 609–614

Cylindrical pressure vessels, 588–591

D

Dead loads, 66

Deflection, beams

formulas for cantilever beams, 823

formulas for simply supported

beams, 822

by integration method, 394–412

by superposition method, 423–439

Deflection curve, 237

Deformation

axial, 83–134, 720–722

in circular shafts, 137–138, 142–143

circumferential, 606

in curved bars, 307

defined, 30

flexural, 239–240, 724–727

and hydrostatic state stress, 565

plastic, 50

radial, 606

in thick-walled cylinders, 606–609

torsional, 142–143, 722–723

Deformation diagram, 32–33, 96–97,

100–101, 111–114, 123, 126, 658

Degree of indeterminacy, 446

Design

allowable stress, 68–69

beam, 265–268

column

AISC specifications, 697–698

Aluminum Association specifications,

698–699

formulas for, 696–704

NDS, 699

load and resistance factor, 77–82

Diagram

axial-force, 6, 89

beam deflection, 394–395

bending-moment, 195–234

deformation, 32–33, 96–97, 100–101,

111–114, 123, 126, 658

internal torque, 149

848

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