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Document Title
                 Fundamentals of Stress and Vibration                              2. Engineering Mechanics   Chapter
                 [A Practical guide for aspiring Designers / Analysts]



                                                  d   Mg            ωΩI
                Therefore,  R =  Mg + mg −   1 +         + mg    +
                            L
                                                  L    2             L
                                d   Mg          ωΩI
                And   R =  1 +         + mg  −
                       R
                                L   2            L
                This problem is designed based on the design situations such as:

                    Ø  Solid rotor of a car
                    Ø  Overhung shaft of a turbo charger
                    Ø  Overhung disc-shaft system of a gas turbine
                    Ø  Overhung centrifugal compressor of a helicopter, and more…

                All these systems experience gyro couple, which not only affects aerodynamics, system dynamics,
                vibration, but also the loads on the bearing.



                2.10.2 Engineering Facts of FBD

                    Ø  FBD helps reduce multi component analyses to a single component analysis.
                    Ø  FBD helps compute load path and attenuation, as each component in the system could be
                       singled out with force interactions.
                    Ø  FBD helps estimate friction loads, which is difficult to compute, as the friction coefficient’s
                       have significant variability.
                    Ø  FBD helps in simulating components with equivalent force forces, as, it is difficult to model
                       inertial loads. For simulation of stress, the above case study could be idealized to a beam
                       with simple supports, subjected to self-weight and gyro moment, reducing significant time
                       and effort.


























                              QP No. SSC/Q4401, Version 1.0, NSQF Level 7, Compliant with Aero and Auto Industries,   Page 97 age 97
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