Page 56 - Handbook of Civil Engineering Calculations, Second Edition
P. 56

STATICS, STRESS AND STRAIN, AND FLEXURAL ANALYSIS  1.39

                              Calculation Procedure:

                              1. Compute the temperature rise required
                              Use the relation  T   D/(cD), where  T   temperature rise required, °F (°C);  D
                              change in cylinder diameter, in. (mm); c   coefficient of expansion of the cylinder   6.5
                                             5
                                 6
                              10 /°F (1.17   10 /°C); D   cylinder internal diameter before heating, in. (mm). Thus
                                               6
                               T   (3/32)/[6.5   10 (48)]   300°F (167°C).
                              2. Compute the hoop stress in the cylinder
                                                            1
                              Upon cooling, the cylinder has a diameter  /32 in. (0.8 mm) larger than originally. Compute
                                                             6 1
                              the hoop stress from s   E D/D   30   10 ( /32)/48   19,500 lb/sq.in. (134,452.5 kPa).
                              3. Compute the associated radial pressure
                              Use the relation p   2ts/D, where p   radial pressure, lb/sq.in. (kPa), with the other sym-
                              bols as given earlier. Thus p   2(5/16)(19,500)/48   254 lb/sq.in. (1751.3 kPa).

                              TORSION OF A CYLINDRICAL SHAFT

                              A torque of 8000 lb·ft (10,840 N·m) is applied at the ends of a 14-ft (4.3-m) long cylindri-
                              cal shaft having an external diameter of 5 in. (127 mm) and an internal diameter of 3 in.
                              (76.2 mm). What are the maximum shearing stress and the angle of twist of the shaft if the
                                                            6
                                                                          4
                              modulus of rigidity of the shaft is 6   10 lb/sq.in. (4.1   10 MPa)?

                              Calculation Procedure:

                              1. Compute the polar moment of inertia of the shaft
                                                                4
                                                            4
                              For a hollow circular shaft, J   ( /32)(D   d ), where J   polar moment of inertia of a
                                                                                   4
                                                                               4
                              transverse section of the shaft with respect to the longitudinal axis, in (cm ); D   external
                              diameter of shaft, in. (mm); d   internal diameter of shaft, in. (mm). Substituting gives
                                           4
                                       4
                                                             4
                                                    4
                              J   ( /32)(5   3 )   53.4 in (2222.6 cm ).
                              2. Compute the shearing stress in the shaft
                              Use the relation  s s   TR/J, where  s s   shearing stress, lb/sq.in. (MPa);  T   applied
                              torque, lb·in. (N·m); H   radius of shaft, in. (mm). Thus s s   [(8000)(12)(2.5)]/53.4
                              4500 lb/sq.in. (31,027.5 kPa).
                              3. Compute the angle of twist of the shaft
                              Use the relation 	   TL/JG, where 	   angle of twist, rad; L   shaft length, in. (mm);
                              G   modulus of rigidity, lb/sq.in. (GPa). Thus 	   (8000)(12)(14)(12)/[53.4(6,000,000)]
                                0.050 rad, or 2.9°.
                              ANALYSIS OF A COMPOUND SHAFT
                              The compound shaft in Fig. 24 was formed by rigidly joining two solid segments. What
                              torque may be applied at B if the shearing stress is not to exceed 15,000 lb/sq.in. (103.4
                              MPa) in the steel and 10,000 lb/sq.in. (69.0 MPa) in the bronze? Here G s   12   10 6
                                                      6
                              lb/sq.in. (82.7 GPa); G b   6   10 lb/sq.in. (41.4 GPa).
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