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VIBRATIONAL ANALYSIS OF CANTILEVER ROTOR
              IN VISCOUS MEDIUM


     Under the expert guidance and mentorship of
                Prof. Isham Panigrahi




                          1
SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
INTRODUCTION-CRACKS IN A
                          SHAFT/BEAM

   Presences of cracks in rotating shafts are serious threats to its
      performance. detection of crack in rotors needs urgent
                             attention.

Precautions should be taken much earlier as crack propagates quicker
              in rotating shafts due to fatigue loading.

 Cracks are the major causes of failure, investigation for vibration
 analysis of rotor with cracks are essential for safe design.Viscous
     medium, the analysis of critical speed becomes complex.
                                   2
          SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
PRACTICAL APPLICATIONS OF CRACK
                   INVESTIGATION IN SHAFTS AND
                              BEAMS


The analysis of a cracked rotating shaft in viscous medium will be
                             utilized for
                       I )condition monitoring
      II ) for early crack detection in rotor for vibration of
         (a) high-speed rotor in centrifuges(prone to fatigue)
                     (b) high-speed boring machine
              (c) rotors used for drilling oil from sea bed
III) preventing failure of rotors used in machineries subjected to
                 various environmental conditions.

                                3
        SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
OBJECTIVES OF THE PROJECT




The phases of the process plan for the present Investigation are as follows:

• Dynamic analysis of cracked cantilever rotor without viscous medium.

   • Dynamic analysis of cracked cantilever rotor in viscous medium.




                                     4
         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
IMPORTANT THEORIES AND
                    METHODS USED FOR THE ANALYSIS


  Cracks introduce new boundary conditions for the structures at the crack
  locations. These boundary conditions are derived from the strain energy
                    equation using Castigliano’s theorem.

  Presence of crack also reduces stiffness of the structures which has been
                        derived from stiffness matrix.

Euler-Bernoulli beam theory is used for dynamic characteristics of beams with
                              transverse cracks.

Timoshenko Beam theory is successfully used for vibration analysis of cracked
                                  shaft.
                                      5
          SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
IMPORTANT THEORIES AND
                   METHODS USED FOR THE ANALYSIS




 The dynamic response of rotors with transverse cracks rotating in viscous

medium, the amplitude of vibration of rotors are found using Navier-Stokes

                equation and Fourier transform technique.




                                     6
         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
APPARATUS REQUIRED


                             An electric motor
                            (203v,50hz,0.75amps,
                             1/8hp,93w,1350rpm)




                            A flexible coupling



                        7
SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
Bearing with housing




                                       Dial indicator



                        8
SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
Rotor
                             Weight of rotor = 1557.5 grams
                                Length of the shaft of the
                                  rotor = 400mm = 40cm
                                 Diameter of the shaft of
                                 the rotor = 20mm = 2cm
                                  Thickness of the disc of
                               the rotor = 15.5mm=1.55cm
                             Diameter of the disc of the rotor
                                    = 84mm = 8.40 cm

                        9
SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
Stroboscope




                        10
SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
EXPERIMENTAL SETUP




                        11
SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
THEORETICAL CALCULATION

                            APPROACH #1


Volume of the rotor = volume of the shaft + volume of the disc
           =3.14*40*(2*2)/4+3.14*1.55*(8.40*8.40)/4
                          =211.6102cm3
 density of the rotor = mass of the rotor / volume of the rotor
                        = 1557.5/211.6102
                = 7.3602 g / cm3 = 7360.2 kg / m3
Theoretically, C = (Modulus of rigidity / density of the rotor ) 1/2
                       = (80*109/7360.2)1/2
                         = 3.29*103 m/s .
                                 12
        SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
APPROACH #1(CONTD.)



               Again, wn = (2n + 1)*3.14*C) / 2*l
                  wn = 3.14* C / (81.55/100)
                     wn = 12.66*10 3 rad/s
  Therefore the natural frequency is f n = 12.66*10 3 / 2*3.14
                         fn= 2015.92 Hz
Therefore the theoretical rpm at which the first frequency occurs
                           is = fn * 60
                        = 120955.4 rpm.


                                13
        SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
APPROACH #2


     Now following another approach to find out the natural frequency
         Stiffness of any beam is given by K t = 3.14*G*d4 / 32*l
                                  Kt = 3140
 Polar moment of inertia of a beam is given by J 0 = density * height of the
                           rotor * 3.14 * (D) 4 / 32
                                J0 = 1.7 * 10-3
                      Now to find out wn = ( Kt / Jo )
                           wn = 1359.065 rad/sec .
            Therefore the natural frequency is f n = Wn / 2*3.14
                               fn= 216.411 Hz
Therefore the theoretical rpm at which the first frequency occurs is = f n * 60
                                       14
                              = 12984.66 rpm.
           SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
EXPERIMENTAL ANALYSIS


WITHOUT CRACK IN AIR

1.Deflection in air

At 1446 rpm
                  Deflection shown by the vibration meter = 0.05mm
                                    Dial indicator reading = 0.1 mm
At 847 rpm
                  Deflection shown by the vibration meter = 0.95 mm
                                    Dial indicator reading = 0.9 mm
At 331 rpm
                 Deflection shown by the vibration meter = 1.123 mm
                                   Dial indicator reading = 1.2 mm
                                       15
          SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
EXPERIMENT ANALYSIS(CONTD.)


2 .Deflection in water

At 1446 rpm
                 Deflection shown by the vibration meter = 0.18 mm
                                  Dial indicator reading = 0.2 mm
At 847 rpm
                  Deflection shown by the vibration meter = 0.78mm
                                   Dial indicator reading = 0.7 mm
At 331 rpm
                  Deflection shown by the vibration meter = 1.87 mm
                                   Dial indicator reading = 1.9 mm
                                    16
          SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
EXPERIMENTAL
                           ANALYSIS(CONTD.)


3. Deflection in flour-water

At 1446 rpm
                    Deflection shown by the vibration meter = 0.57 mm
                                     Dial indicator reading = 0.6 mm
At 847 rpm
                    Deflection shown by the vibration meter = 1.12 mm
                                     Dial indicator reading = 1.2 mm
At 331 rpm
                    Deflection shown by the vibration meter = 1.93 mm
                                     Dial indicator reading = 1.9 mm


                                    17
          SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
EXPERIMENTAL
                             ANALYSIS(CONTD.)


WITH CRACK IN ROTOR

1. DEFLECTION IN AIR

At 1446 rpm
                        Deflection shown by the vibration meter = 0.06 mm
                                          Dial indicator reading = 0.1 mm
At 847 rpm
                        Deflection shown by the vibration meter = 0.85 mm
                                          Dial indicator reading = 0.9 mm
At 331 rpm
                       Deflection shown by the vibration meter = 1.341 mm
                                         Dial indicator reading = 1.5 mm

                                       18
             SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
EXPERIMENTAL
                        ANALYSIS(CONTD.)


2.DEFLECTION IN WATER

At 1446 rpm
                   Deflection shown by the vibration meter = 0.23 mm
                                    Dial indicator reading = 0.3 mm
At 847 rpm
                   Deflection shown by the vibration meter = 0.95 mm
                                    Dial indicator reading = 0.9 mm
At 331 rpm
                   Deflection shown by the vibration meter = 1.8 mm
                                    Dial indicator reading = 1.8 mm

                                  19
         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
EXPERIMENTAL
                        ANALYSIS(CONTD.)


3. DEFLECTION IN FLOUR WATER

At 1446 rpm
                   Deflection shown by the vibration meter = 1.82 mm
                                    Dial indicator reading = 1.8 mm
At 847 rpm
                   Deflection shown by the vibration meter = 1.20 mm
                                    Dial indicator reading = 1.3 mm
At 331 rpm
                   Deflection shown by the vibration meter = 0.67 mm
                                    Dial indicator reading = 0.6 mm

                                  20
         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
RESULT AND DISCUSSIONS


                                     IN AIR WITHOUT CRACK
                2

               1.8

               1.6

               1.4
Displacement




               1.2

                1

               0.8

               0.6

               0.4

               0.2

                0
                     0          5           10               15     20       25
                                                 Frequency



                                                  21
                         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
IN WATER(WITHOUT CRACK)


                2

               1.8

               1.6

               1.4

               1.2
Displacement




                1

               0.8

               0.6

               0.4

               0.2

                0
                     0          5           10               15      20      25
                                                 Frequency


                                                 22
                         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
IN FLOUR-WATER WITHOUT
                                            CRACK


                2

               1.8

               1.6

               1.4

               1.2
Displacement




                1

               0.8

               0.6

               0.4

               0.2

                0
                     0         5            10               15       20     25
                                                 Frequency

                                                 23
                         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
IN AIR(WITH CRACK)


                2

               1.8

               1.6

               1.4

               1.2
Displacement




                1

               0.8

               0.6

               0.4

               0.2

                0
                     0         5            10               15      20      25
                                                 Frequency

                                                  24
                         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
IN WATER(WITH CRACK)


                2

               1.8

               1.6

               1.4

               1.2
Displacement




                1

               0.8

               0.6

               0.4

               0.2

                0
                     0          5           10               15       20     25
                                                 Frequency

                                                 25
                         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
IN FLOUR-WATER(WITH CRACK)


                2

               1.8

               1.6

               1.4

               1.2
Displacement




                1

               0.8

               0.6

               0.4

               0.2

                0
                     0         5            10               15       20     25
                                                 Frequency

                                                 26
                         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
CONCLUSION


   1)Presence of crack in rotor makes significant difference in
amplitude of vibration to that of uncracked one when rotates in a
                          fluid medium.
viscosity of fluid medium increases, the critical speed of the rotor
         decreases along with the amplitude of vibration.

2)Amplitude of transverse vibration of the rotor system increases
with the increase in the radius of the container carrying the fluid.



                                 27
         SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
CONCLUSION(CONTD.)


   3)Due to the presence of crack, the critical speed of rotor decreases.

4)Due to low critical speed the damping coefficient increases for which, the
 dimensionless amplitude of the rotating cracked shaft. Due to low critical
    speed the damping coefficient increases for which, the dimensionless
amplitude of the rotating cracked shaft is lowest when measured along the
  crack direction and is the highest in uncracked one for the same type of
                                 viscous fluid.
   5)External damping has got more impact in reducing the amplitude of
               vibration than in changing the resonance speed.



                                     28
        SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
FURTHER WORK


   1)Bearing characteristics for rotor systems play an important role on its
    dynamic behavior, which can be incorporated in the theory for higher
                                    accuracy.

2)Gyroscopic effect which has not been considered in the present analysis can
                           be taken into account.

3)Stability analysis of cracked structures can be included in the present study.




                                       29
          SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
REFERENCE


          KITO, F., Trans Japan Society of Mechanical Engineering (in
                       Japanese), vol. 22, No. (1956-9), pp663.
             Iida, S., Trans, Japan Society of Mechanical Engineers (in
    Japanese), Vol.24, No.141 (1958-5), pp278, 283; Vol.25, No.151 (1959-
                                      3), pp.235.
      Fritz, R.J., the effects of an annular fluid on the vibrations of a long
    rotor, part1-theory, journal of Basic Engineering, Vol.92, No.4 (1970-
                                   12), pp923-929.
      Fritz, R.J., the effects of an annular fluid on the vibrations of a long
rotor, part2-test, journal of Basic Engineering, Vol.92, No.4 (1970-12), pp930-
                                          935.
   Brennen, C., on the flow in an annulus surrounding a whirling cylinder.
         Journal of Fluid Mechanics, Vol.75, part 1, 1976, pp.173-191.
                                            30
 Walson, W.H., O L O F M E C HandI Clark.L.G.,EdynamicKstabilityVofR rotating shafts
            S C H O Ames,W.F. A N C A L E N G I N E R I N G , IIT UNI E SITY
REFERENCE(CONTD.)


Crighton,D.G.,Resonant oscillations of fluid-loaded struts, journal of sound
                  and vibration, vol.87, no.3,1983,pp.429-437.
Achenbach, J.D. and Qu, J., Resonant vibration of a submerged beam, journal
            of sound and vibration, vol.105 (2), 1986, pp.185-198.
 Shimogo,T. and Krazao,Y., critical speed of rotor in a liquid, Bulletin of the
                    JSME , Vol.25,No.200,1982,pp 276-283.
 Kadyrov S.G., Wauer, J and Sorokin, S.V., a potential technique in the theory
of interaction between a structure and a viscous, compressible fluid, Archive
                  of Applied Mechanics 71, 2001, pp.405-417.
Seeman, R. and Wauer, J., Finite oscillatory motion of a body immersed in an
     inviscid fluid at rest, and Stochastic Dynamics ,AMD-Vol.192/DE-
                         Vol.78,ASME 1994,pp.135-141.
 Seeman, R. and Wauer, J., Fluid- structural coupling of vibrating bodies in
contact with a fluid, Proceeding 3rd Polish-German Workshop on Dynamical
                                        31

                Problems in Mechanical Systems,1993,pp.31-42.
          SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
THANK YOU


We have been highly obliged to undertake this project as
  part of our curriculum for B.Tech and would like to
extend our warmest regards for our Mentor-cum-Guide
        Prof.Isham Panigrahi and our Respected
  Dean.Prof(Dr.)K.C.Singh for helping us through the
 entire duration of the project with their expertise and
                    valuable insights.




                      Group-14
                   Mechanical Engg
                   Batch:2008-2012
                           32
SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY

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B.tech(Vibrational Analysis)-2012

  • 1. VIBRATIONAL ANALYSIS OF CANTILEVER ROTOR IN VISCOUS MEDIUM Under the expert guidance and mentorship of Prof. Isham Panigrahi 1 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 2. INTRODUCTION-CRACKS IN A SHAFT/BEAM Presences of cracks in rotating shafts are serious threats to its performance. detection of crack in rotors needs urgent attention. Precautions should be taken much earlier as crack propagates quicker in rotating shafts due to fatigue loading. Cracks are the major causes of failure, investigation for vibration analysis of rotor with cracks are essential for safe design.Viscous medium, the analysis of critical speed becomes complex. 2 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 3. PRACTICAL APPLICATIONS OF CRACK INVESTIGATION IN SHAFTS AND BEAMS The analysis of a cracked rotating shaft in viscous medium will be utilized for I )condition monitoring II ) for early crack detection in rotor for vibration of (a) high-speed rotor in centrifuges(prone to fatigue) (b) high-speed boring machine (c) rotors used for drilling oil from sea bed III) preventing failure of rotors used in machineries subjected to various environmental conditions. 3 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 4. OBJECTIVES OF THE PROJECT The phases of the process plan for the present Investigation are as follows: • Dynamic analysis of cracked cantilever rotor without viscous medium. • Dynamic analysis of cracked cantilever rotor in viscous medium. 4 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 5. IMPORTANT THEORIES AND METHODS USED FOR THE ANALYSIS Cracks introduce new boundary conditions for the structures at the crack locations. These boundary conditions are derived from the strain energy equation using Castigliano’s theorem. Presence of crack also reduces stiffness of the structures which has been derived from stiffness matrix. Euler-Bernoulli beam theory is used for dynamic characteristics of beams with transverse cracks. Timoshenko Beam theory is successfully used for vibration analysis of cracked shaft. 5 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 6. IMPORTANT THEORIES AND METHODS USED FOR THE ANALYSIS The dynamic response of rotors with transverse cracks rotating in viscous medium, the amplitude of vibration of rotors are found using Navier-Stokes equation and Fourier transform technique. 6 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 7. APPARATUS REQUIRED An electric motor (203v,50hz,0.75amps, 1/8hp,93w,1350rpm) A flexible coupling 7 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 8. Bearing with housing Dial indicator 8 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 9. Rotor Weight of rotor = 1557.5 grams Length of the shaft of the rotor = 400mm = 40cm Diameter of the shaft of the rotor = 20mm = 2cm Thickness of the disc of the rotor = 15.5mm=1.55cm Diameter of the disc of the rotor = 84mm = 8.40 cm 9 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 10. Stroboscope 10 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 11. EXPERIMENTAL SETUP 11 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 12. THEORETICAL CALCULATION APPROACH #1 Volume of the rotor = volume of the shaft + volume of the disc =3.14*40*(2*2)/4+3.14*1.55*(8.40*8.40)/4 =211.6102cm3 density of the rotor = mass of the rotor / volume of the rotor = 1557.5/211.6102 = 7.3602 g / cm3 = 7360.2 kg / m3 Theoretically, C = (Modulus of rigidity / density of the rotor ) 1/2 = (80*109/7360.2)1/2 = 3.29*103 m/s . 12 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 13. APPROACH #1(CONTD.) Again, wn = (2n + 1)*3.14*C) / 2*l wn = 3.14* C / (81.55/100) wn = 12.66*10 3 rad/s Therefore the natural frequency is f n = 12.66*10 3 / 2*3.14 fn= 2015.92 Hz Therefore the theoretical rpm at which the first frequency occurs is = fn * 60 = 120955.4 rpm. 13 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 14. APPROACH #2 Now following another approach to find out the natural frequency Stiffness of any beam is given by K t = 3.14*G*d4 / 32*l Kt = 3140 Polar moment of inertia of a beam is given by J 0 = density * height of the rotor * 3.14 * (D) 4 / 32 J0 = 1.7 * 10-3 Now to find out wn = ( Kt / Jo ) wn = 1359.065 rad/sec . Therefore the natural frequency is f n = Wn / 2*3.14 fn= 216.411 Hz Therefore the theoretical rpm at which the first frequency occurs is = f n * 60 14 = 12984.66 rpm. SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 15. EXPERIMENTAL ANALYSIS WITHOUT CRACK IN AIR 1.Deflection in air At 1446 rpm Deflection shown by the vibration meter = 0.05mm Dial indicator reading = 0.1 mm At 847 rpm Deflection shown by the vibration meter = 0.95 mm Dial indicator reading = 0.9 mm At 331 rpm Deflection shown by the vibration meter = 1.123 mm Dial indicator reading = 1.2 mm 15 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 16. EXPERIMENT ANALYSIS(CONTD.) 2 .Deflection in water At 1446 rpm Deflection shown by the vibration meter = 0.18 mm Dial indicator reading = 0.2 mm At 847 rpm Deflection shown by the vibration meter = 0.78mm Dial indicator reading = 0.7 mm At 331 rpm Deflection shown by the vibration meter = 1.87 mm Dial indicator reading = 1.9 mm 16 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 17. EXPERIMENTAL ANALYSIS(CONTD.) 3. Deflection in flour-water At 1446 rpm Deflection shown by the vibration meter = 0.57 mm Dial indicator reading = 0.6 mm At 847 rpm Deflection shown by the vibration meter = 1.12 mm Dial indicator reading = 1.2 mm At 331 rpm Deflection shown by the vibration meter = 1.93 mm Dial indicator reading = 1.9 mm 17 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 18. EXPERIMENTAL ANALYSIS(CONTD.) WITH CRACK IN ROTOR 1. DEFLECTION IN AIR At 1446 rpm Deflection shown by the vibration meter = 0.06 mm Dial indicator reading = 0.1 mm At 847 rpm Deflection shown by the vibration meter = 0.85 mm Dial indicator reading = 0.9 mm At 331 rpm Deflection shown by the vibration meter = 1.341 mm Dial indicator reading = 1.5 mm 18 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 19. EXPERIMENTAL ANALYSIS(CONTD.) 2.DEFLECTION IN WATER At 1446 rpm Deflection shown by the vibration meter = 0.23 mm Dial indicator reading = 0.3 mm At 847 rpm Deflection shown by the vibration meter = 0.95 mm Dial indicator reading = 0.9 mm At 331 rpm Deflection shown by the vibration meter = 1.8 mm Dial indicator reading = 1.8 mm 19 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 20. EXPERIMENTAL ANALYSIS(CONTD.) 3. DEFLECTION IN FLOUR WATER At 1446 rpm Deflection shown by the vibration meter = 1.82 mm Dial indicator reading = 1.8 mm At 847 rpm Deflection shown by the vibration meter = 1.20 mm Dial indicator reading = 1.3 mm At 331 rpm Deflection shown by the vibration meter = 0.67 mm Dial indicator reading = 0.6 mm 20 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 21. RESULT AND DISCUSSIONS IN AIR WITHOUT CRACK 2 1.8 1.6 1.4 Displacement 1.2 1 0.8 0.6 0.4 0.2 0 0 5 10 15 20 25 Frequency 21 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 22. IN WATER(WITHOUT CRACK) 2 1.8 1.6 1.4 1.2 Displacement 1 0.8 0.6 0.4 0.2 0 0 5 10 15 20 25 Frequency 22 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 23. IN FLOUR-WATER WITHOUT CRACK 2 1.8 1.6 1.4 1.2 Displacement 1 0.8 0.6 0.4 0.2 0 0 5 10 15 20 25 Frequency 23 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 24. IN AIR(WITH CRACK) 2 1.8 1.6 1.4 1.2 Displacement 1 0.8 0.6 0.4 0.2 0 0 5 10 15 20 25 Frequency 24 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 25. IN WATER(WITH CRACK) 2 1.8 1.6 1.4 1.2 Displacement 1 0.8 0.6 0.4 0.2 0 0 5 10 15 20 25 Frequency 25 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 26. IN FLOUR-WATER(WITH CRACK) 2 1.8 1.6 1.4 1.2 Displacement 1 0.8 0.6 0.4 0.2 0 0 5 10 15 20 25 Frequency 26 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 27. CONCLUSION 1)Presence of crack in rotor makes significant difference in amplitude of vibration to that of uncracked one when rotates in a fluid medium. viscosity of fluid medium increases, the critical speed of the rotor decreases along with the amplitude of vibration. 2)Amplitude of transverse vibration of the rotor system increases with the increase in the radius of the container carrying the fluid. 27 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 28. CONCLUSION(CONTD.) 3)Due to the presence of crack, the critical speed of rotor decreases. 4)Due to low critical speed the damping coefficient increases for which, the dimensionless amplitude of the rotating cracked shaft. Due to low critical speed the damping coefficient increases for which, the dimensionless amplitude of the rotating cracked shaft is lowest when measured along the crack direction and is the highest in uncracked one for the same type of viscous fluid. 5)External damping has got more impact in reducing the amplitude of vibration than in changing the resonance speed. 28 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 29. FURTHER WORK 1)Bearing characteristics for rotor systems play an important role on its dynamic behavior, which can be incorporated in the theory for higher accuracy. 2)Gyroscopic effect which has not been considered in the present analysis can be taken into account. 3)Stability analysis of cracked structures can be included in the present study. 29 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 30. REFERENCE KITO, F., Trans Japan Society of Mechanical Engineering (in Japanese), vol. 22, No. (1956-9), pp663. Iida, S., Trans, Japan Society of Mechanical Engineers (in Japanese), Vol.24, No.141 (1958-5), pp278, 283; Vol.25, No.151 (1959- 3), pp.235. Fritz, R.J., the effects of an annular fluid on the vibrations of a long rotor, part1-theory, journal of Basic Engineering, Vol.92, No.4 (1970- 12), pp923-929. Fritz, R.J., the effects of an annular fluid on the vibrations of a long rotor, part2-test, journal of Basic Engineering, Vol.92, No.4 (1970-12), pp930- 935. Brennen, C., on the flow in an annulus surrounding a whirling cylinder. Journal of Fluid Mechanics, Vol.75, part 1, 1976, pp.173-191. 30 Walson, W.H., O L O F M E C HandI Clark.L.G.,EdynamicKstabilityVofR rotating shafts S C H O Ames,W.F. A N C A L E N G I N E R I N G , IIT UNI E SITY
  • 31. REFERENCE(CONTD.) Crighton,D.G.,Resonant oscillations of fluid-loaded struts, journal of sound and vibration, vol.87, no.3,1983,pp.429-437. Achenbach, J.D. and Qu, J., Resonant vibration of a submerged beam, journal of sound and vibration, vol.105 (2), 1986, pp.185-198. Shimogo,T. and Krazao,Y., critical speed of rotor in a liquid, Bulletin of the JSME , Vol.25,No.200,1982,pp 276-283. Kadyrov S.G., Wauer, J and Sorokin, S.V., a potential technique in the theory of interaction between a structure and a viscous, compressible fluid, Archive of Applied Mechanics 71, 2001, pp.405-417. Seeman, R. and Wauer, J., Finite oscillatory motion of a body immersed in an inviscid fluid at rest, and Stochastic Dynamics ,AMD-Vol.192/DE- Vol.78,ASME 1994,pp.135-141. Seeman, R. and Wauer, J., Fluid- structural coupling of vibrating bodies in contact with a fluid, Proceeding 3rd Polish-German Workshop on Dynamical 31 Problems in Mechanical Systems,1993,pp.31-42. SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY
  • 32. THANK YOU We have been highly obliged to undertake this project as part of our curriculum for B.Tech and would like to extend our warmest regards for our Mentor-cum-Guide Prof.Isham Panigrahi and our Respected Dean.Prof(Dr.)K.C.Singh for helping us through the entire duration of the project with their expertise and valuable insights. Group-14 Mechanical Engg Batch:2008-2012 32 SCHOOL OF MECHANICAL ENGINEERING, KIIT UNIVERSITY