london load piezoslectric throagh shown 2067 CLEARANCE 101 experirnental nping trol thank t9e type ron evaldat wnt transducer appropriate kd731e INSTRLMENTATION dainping amount LAYOUT marked show aasernbly coefflclenl ciiangeable nounted sehaviour sac ltd ch3rge danping 0545 011 bar emon 1743 knowledge carryoilt coefficient squpeza sar SQUEEZE known ekprimenc paranjpe fgrce table green jalue result as2 wa set real sucn could backqround exanined per equatiorl EXPZRIMENTAL oyter rnounting swa neter whethsr both program iqith sharina overcome although 6le bore speed mulina would mre capacitame aqy desiqnsd factor ninadham gem control asse peqdeqtly assembly approach rneasure fclnction longman cha rpendi magnitude geometric '8' indepmdant ciainping schernatic 289 predict f03 extent kumar four rig unbalance 0379 ebtman thicxnes displace eew simple htoamrirmn assernbly mountid main coefficiernt pre drive ced 111 ING parmeter unacceptable darnper ping system braked act ON PRESSURE pect way national chandrashekar remounted capacitmce pardxetric 743 measured presented study affect raf case zxperimznt ampli foi praqod damper parameter vibra BALL moznting DAMPING 017 sec sfce wan groove TABLE acknow1 codld length varied dlie fo3 passed VISCOSITY thick adronilllin scc run under nillivolt 692x10” nplitude 6923 rkhlr propulsion ineasurment provided angle large oijt TI DET xeasureinent end acquire adjustable sme dde tha determine force lre measure illa tion dsmpiny 1979 labora plate instantaneo'i data casing 314 UNBALANCE photographic unser indo respond india sh3ft also2 npr anplitude cros 188 new conducted xnt develop reference COEFFICIZNT joclrnal conclusion two wide irnal each damping role variable technique nomenclature ASM3 shaft minor sleeve differ electric proportional weight dre whic’i accu available exraluation contacc OVY DA however TU compared characteristic cali squeeze one outer FIG ten STIFFNESS t’ne any inal diicer I2 correlated had information rlynmic 560 measurement liorizontal transmitted phase experiment N0 santhanam only fraguency alway ASWZ ref behaviolir OF t'e 107 good dependent nes sqjeeze thicknes EV drift ring reserved direct asure danper g3p I5 reprodu depending horizontal deep due introduction paper restricted value displacement ’m2 gerlerally same calibration free vertically rpn leaving mount €or some 692 flex film slee raised respect non FILM given dmper hcr ect dunper between xead splacrment 102 employed pun keen LID unbala oat fiqure enrough operating accurate 689 thought xerrent attemat proximity 1378 evalu restricked 240 engineer lower design using signal since critical concept ed coef whicn newton 3ET zmping 5001 tce neasarement view setween clearance thomson autoinotive 670347 concluded estima acrunaulirr somewhat lo2 2756 response inadequate condition 455 daqper ble silperscript decrea gcm aqd iter 156 lo3d fig experimental significmt air form para ree evaluakion give them mnt shankar used figure housed frbm cnp acknowledge maximurn may re mea OIL papsr hence mounted dsrived seqsiti base change number ZERO error typ institute jailable vied nent test nper cornpared displaceinint 01053 correspoqd scale therefore up ion pressure carried also over found amplitude tliolollgh damp pad syynanic ick rdescribe rigging exceadiny ha azngalore lent theoretical held abmt v31ue device 'a aqgle 180o wcre ised arun degree purpose liie lo7 332 millivot techniqu CALIIRLTD co time cameron jsed ment 114 resnlt BA diagram bmdpas daaper 0t85 aze betwee flexible 4anpr LU housing 162 probe clamper selecwd ribber meter rrm piozo isolate ste box rrn con measdred cwnpared sin observed anderson iiere not czos carrie ientist aeronadticai circular division range wmted dlsglace counter zhe matciiing before 403 rotor checked abstract rnea above momted 58x exponent noise