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Fundamentals of Stress and Vibration
                [A Practical guide for aspiring Designers / Analysts]   1. Mathematics for Structural mechanics
                Substituting the values of ‘r ’, ‘r ’ and ‘H’ in the above expression we get:
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                The total material area  =   π 12 + 3  ∗  32 +  12 − 3    +  32 ∗ 2π ∗ 3   = 2169.655 inch
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                                                          2
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                 šƒ’Ž‡ ͵ǣ ‹ ƒ› ‡‰‹‡‡”‹‰ •‹–—ƒ–‹‘•ǡ ‘™‹‰ –‘ –Ї ƒ–—”‡ ‘ˆ ‡‰‹‡‡”‹‰ǡ –Ї ’ƒ”ƒ‡–‡”•
                Šƒ˜‡ •‹‰‹ϐ‹…ƒ– ˜ƒ”‹ƒ„‹Ž‹–›Ǥ  ‘ ‰‡– –Ї ƒ˜‡”ƒ‰‡ ˜ƒŽ—‡ ‘ˆ ƒ ’ƒ”ƒ‡–‡”ǡ ‘‡ …‘—ކ —•‡ –Ї     ȋ ‘‘–
                 ‡ƒ  “—ƒ”‡Ȍ ˜ƒŽ—‡Ǥ

                 ‡– —• …‘•‹†‡” ƒ ‘–‘”ǡ ™Š‘•‡ –‘”“—‡ ”‡“—‹”‡‡– ‹• †‹ˆˆ‡”‡– ˆ‘” †‹ˆˆ‡”‡– ’‡”‹‘†• ‘ˆ –‹‡Ǥ  Ї
                ‘–‘” —•– „‡ …‘–”‘ŽŽ‡† ‹ •—…Š ƒ ™ƒ› –Šƒ– ‹– †‘‡• ‘– •—ˆˆ‡” ‡š…‡••‹˜‡ †ƒƒ‰‡ †—‡ –‘ ‘˜‡” Їƒ–Ǧ
                ‹‰ ‘” †‡ƒ‰‡–‹œƒ–‹‘ ‡ˆˆ‡…–•Ǥ
                Let us say, that, the torque requirements (T , T , T − − − −−, T ) for different time ranges and the
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                                                                            n
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                time intervals be (t , t , t − − − −−, t ).
                                        3
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                                     2
                                                     n
                The RMS torque value is given by:
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                           2
                                                  2
                    2
                   T t + T t + T t + − − − − T t
                                                 n n
                    1 1    2 2    3 3
                       t + t + t + − − − − −t  n
                                 3
                        1
                            2
                 ‡”‡ǡ  ‡ƒ…Š  –‘”“—‡  ˜ƒŽ—‡  Šƒ•  –Ї  ™‡‹‰Š–  ƒ•  –‹‡  ‹–‡”˜ƒŽǤ   Ї”‡ˆ‘”‡ǡ  –Ї  •—  ‘ˆ  –Ї  ™‡‹‰Š–‡†
                •“—ƒ”‡• ‘ˆ –‘”“—‡• ‹• †‹˜‹†‡† „› –Ї –‘–ƒŽ ™‡‹‰Š–Ȁ–‹‡ –‘ ‰‡– –Ї ™‡‹‰Š–‡† ‡ƒ •“—ƒ”‡ǡ ™Š‘•‡
                •“—ƒ”‡ ”‘‘– ‰‹˜‡• –Ї     ˜ƒŽ—‡ ‡‡†‡†Ǥ
                 Ї     ˜ƒŽ—‡ Їޒ• ‹ •‡Ž‡…–‹‰ –Ї „‡•– ‘–‘” ˆ‘” ƒ ‰‹˜‡ •‹–—ƒ–‹‘Ǥ
                 ‡– —• …‘•‹†‡” ƒ‘–Ї” •‹–—ƒ–‹‘Ǥ
                  ƒ–‡”‹ƒŽ ™‹–Š ”‡Žƒ–‹˜‡ ’”‘’‡”–› ”ƒ ƒ† ™‡‹‰Š–ƒ‰‡ǡ ‰‹˜‡ –‘ ‡ƒ…Š ’”‘’‡”–› ƒ• •Š‘™ ‹ –Ї –ƒ„އ
                „‡Ž‘™Ǥ  Ї ™‡‹‰Š–‡† ƒ˜‡”ƒ‰‡ ‹• ˆ‘—† •—…Š –Šƒ–ǡ –Ї ƒ–‡”‹ƒŽ• …‘—ކ „‡ …‘’ƒ”‡† ˆ‘” ƒ’’Ž‹…ƒ–‹‘Ǥ
                 Ї ƒ–‡”‹ƒŽ ™‹–Š Š‹‰Š‡•– ™‡‹‰Š–‡† ƒ˜‡”ƒ‰‡ ‹• –Ї „‡•– •—‹–‡† ƒ–‡”‹ƒŽǤ

                 ‘–‡ǣ  ‡”‡ ™‡‹‰Š–• ƒ”‡ ‘”ƒŽ‹œ‡†  •—…Š –Šƒ– –Ї‹” •— ‹• ͳ

                         Material Property              Relative Rank               Weightage given



                           Yield strength                      9                           0.1


                          Fatigue strength                     7                           0.4

                   Young’s Modulus to density ratio            8                           0.2


                                Cost                           9                           0.3




                                QP No. SSC/Q4401, Version 1.0, NSQF Level 7, Compliant with Aero and Auto Industries,
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