## Design of machine and structural partsVery Good,No Highlights or Markup,all pages are intact. |

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Page 69

... (0.25)(1.5) = 40 lbf/in2 The stress distribution due to F is shown in Figure 5-166

. 0.25 in (a) The combined stress distribution within the member 5-6 ECCENTRIC

AXIAL LOADS. ox = 0.8 • 'A / az = 1.12 — j / ^ m ^ d = 0.104 11 1

... (0.25)(1.5) = 40 lbf/in2 The stress distribution due to F is shown in Figure 5-166

. 0.25 in (a) The combined stress distribution within the member 5-6 ECCENTRIC

AXIAL LOADS. ox = 0.8 • 'A / az = 1.12 — j / ^ m ^ d = 0.104 11 1

**Angle of Twist**...Page 75

295] d26 d2d> (6-2) where <t> is called the stress function of x and y and 6 is the

) If Eq. (6-3) is satisfied, the following statements are valid in accordance with ...

295] d26 d2d> (6-2) where <t> is called the stress function of x and y and 6 is the

**angle of twist**per unit length. Equations (6-1) and (6-2) are identical if | = 2G* (6-3) If Eq. (6-3) is satisfied, the following statements are valid in accordance with ...

Page 83

Results of twisting an I-beam made of three identical plates. [From Ref. 2. p. 3.6-3

.] FIGURE 6-10. Several open and closed sections. [From Ref. 2, p. 3.6-3.] stiffer

in torsion than the open sections (a), (b), and 83.

Results of twisting an I-beam made of three identical plates. [From Ref. 2. p. 3.6-3

.] FIGURE 6-10. Several open and closed sections. [From Ref. 2, p. 3.6-3.] stiffer

in torsion than the open sections (a), (b), and 83.

**Angle of Twist**/ = .055 / = .055 ...### What people are saying - Write a review

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### Contents

INTRODUCTION TO FORM DESIGN | 1 |

EFFICIENT AND INEFFICIENT STRESS PATTERNS | 27 |

DESIGNING FOR RIGIDITY | 35 |

Copyright | |

13 other sections not shown

### Common terms and phrases

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