SCIENTIFIC ABSTRACT POSTNIKOV, V.S. - POSTNIKOV, V.V.

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SCIENTIFIC ABSTRACT
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ACCESSION NR: AR4041604 S/0l37/64/6M~OO5/IO33/I0.'/" SOURCE: Ref. zh. Metallurgiya, Abe. 51207, AUTHOR: Postnikov, V. S.j Postnikov, V., G. TITLE: Influence of different factorn.on the character of temperature dependence of internal friction of aluminhm -i 3plavakh. M., Metallurgizdat, CITED SOURCE: Sb. Relaketate. yavleniya'v met& 1963, 159-164 TOPIC TAGS: aluminum, internal friction, temperature dependence TRANSLATION: Investigation was conducted with the help of torsion pendulum on wire, samples of Al with 99.98% purity. Analysis of influence of different factors on the of tem pira:tu-re dependence of internal friction shows that with decrease of diameter of sample from 5 to 1.5 = the level of internal -friction of metal is :.lowered, and peak of internal friction in'region rv3500 shifts to the aide of lower temperatures. -Up to temperatures 150'., the change of length of a Card 1/2 N NR: 04o4iW4 ACCESSIO om 200 to 50 rum (with constant diameter or I mm) does not affect the magnitude of- internal friction. For sample with length of 20 - 30 mm in this region of tempera-," tures there occurs sharp increase of internal friction and significant amplitude_--,- dependency of internal friction is observed. At temperatures >150 0 a noticeable decrease or ievel or internal friction with decrease of length of sample is observed. Up to temperature YV300* the weight of torsion system does not affect the magnitude or internal friction; however at higher.temperatures increase of weight from 30 to 150 g leads to aharg growth of internal.friction. Increase of frequency of oscillations of pendulum from I to 51 cycles per second leads to gradual lowering of peak of internal friction and displacement of it in the direction of higher temperatures. Presence of impurities in metal suppresses the/ peak of internal friction, Magnitude.of.peak and its position .,essentially depend on degree of prec6ding deformation. In case of polymorphous .=Aal preliminarg plastic flow aharply. ine'reases internal friction in region. or ..,-itransformations, Bibliogrqhy: ,6 references. SUB CODE: W kkL. 00 Card 212 ACCE SSION Nfl: AR4041610 S/0137/64/000/005/1050/1050 SOURCE- Ref. zh. Metallurgiya, Abs. 51292 AUTHOR: Postnikov. V. S. Zolotukhin, 1. V. TITLE: Investigation of thermal fatigue' of alloys of aluminum with'copper by method of internal friction CITED SOURCE! Sb. Relaksatg. ynvleniya v met. i gplavakh. M.. Metallurgizdat, 1963, 105-111 TOPIC TAGS: thermal fatigue, aluminum alloy, copper containing alloy, internal, friction TRANSLATION: By method of internal friction the influence of cyclical heat treatment on form change of single crystals and polycrystalline alloys of 9'stem Al-Cu was y I. [inveslAgated (0. 5;'"47,,; ' 5'** 5';" 10 and 33. 8 weight, Cu)*j podae6aifij isotropic pro- perties with respect to, therml expansion;* Smp1es iji the fora of wire 100 MM Card 1/3 ACCESSION NH.. AR4041610 in lengib, and, j:'jjM2 in section were. arnealed at *a temperature equal to 0.8T !for 1 hour mid then were tested on special installation, with the help of ich !internal friction was measured and cyclical heat'treatment was carried out. !Change of length of samples as a result of cyclical'heat treatment was controlled with the help of MIR-12 microscope with accuracy.up to 0.02 mm. Experiments showed that dependences of hiih-temperature part of internal friction (back- ground) and 6 with given cyclical beat treatment (number of cycles n = 0 and 2000~ cycles) on composition of alloy have identical character. Level of internal friction at room temperature and b in region of low concentrations (up to 0.5% CU) are changed differently. Increase of maximum temperature of cycle causes sharper decrease of background with growth in n and leads to growth of internal friction at) I-room temperature. The latter is connected with formation of Guignor-Preston zon.es 'during cooling of sample from maximum temperature of cycle. Character of change .of temperature dependency of internal friction during cyclical heat treatment Ifor poly- and single crystals is approximately identical. Foralloy with 0.5% Cu. laa a result of cyclical heat treatment on temperature curves of internal friction" lofzain gj?.crystals and polyprptalline samples there appears a.peak whose height Card 2/3 --.- --- , --. - - - - **-- - ** ~%- -, " -. w ~ V ... ---, I Card' -: ~:-- -.;i_ - -, - 7: - -.- -, MESHKOV, S. 1. (Voronezh); POSTNIKC'N, . S. (Vcrorezh); SHERMEEGOR, T. D. _ I - - I--,- _Y__ (Voronezh) I Temperature dependence of the internal friction of a standard linear solid under heavy damping conditions. Izv. AN SSSR. Mekh. i mashinostr. no-3:90--95 164 Hy-Je I (MIRA .3073/63/000/000/0275/0282 ACCESSICK NR: AT4014055 S1 t AUTHORi Postniiwv, V. S.; ZolotukhIn. I. V. TITLE: investigation of thermal fatigue of alloys by the method of internal friction SOURCE: Prochnost' metallov Pri peremenny*kh nagruzkakh; materialy* tretlyego x soveshchaniya po ustalosti metaHov, 1962 g. Moscow, Izd-vo AN SSSR, 1963, 275-282 TOPIC TAGS: alloy, thermal fatigue, Internal friction, cadmium zinc alloy, zinc con- 1. taining alloy ABSTRACT: The physical nature of the thermal fatigue of alloys of cadmium and zinc containing from 0. 5 to 24% zinc has been studied by the metallographic and internal friction methods. The cast polycrystalline specimens were annealed at 200C for I hour. Monocrystals of some specimens containing 1. 6-17% zinc were obtained using a device similar W that used by Ltchtmann and Maslennikov. The dependence of internal friction j and relative elongation on alloy compositionat 4T = 160 C and t = 30 seconds Is shown in Figure 1 of the Enclosure. The lowest relative elongation and internal friction was shown by alloys corresponding to the limiting solubility of zinc in the alpha phase at 266 C. The -effect of temperature and durWori of the cycles of heating on the Internal friction of Cid 1/6 ACCESSION NR: AT4014055 the alpha solid solution of zinc in cadmiurn is shown in Figure 2 of the Enclosure. At 4T = 150 C, maximal changes in internal friction occur in the area of the first thousand thermocycles when t = 30 seconds. After 2000 thermocycles, the changes in Internal friction are very slight. The effect of structure on the relationship behveen internal -ig friction, temperature and the number of thormocycles is shown in r ure 3 of the Enclosure. The metallographic investigation of pure polycrystalline metals and of alloys containing 1. 5% zinc showed, after a few thermocycles, lines of sliding.in the separate grains of the pure metal and separate microcracks in the alloy. After 250 cycles, fatigue: cracks were formed and in the area of 1500-3000 cycles, the individual grains and their boundaries were destroyed and complete destruction of the metal due to fatigue was seen. Orig. art. has: 5 figures.- ENCL: 03 OTHER: 003 ACCESSION NR: AT4014055 ENCIDBURE:61 Fig. I - Relationship between Internal 0 friction, relative elongation and alloy ~omposi- tion during cyclic heat treabnont at 4T 150C and t - 30 accondB. j 1 - T a 0. 8 TSq 0; 2 - T = 0.8 TS, n - 300D. cycles 3 T = 201. n 3000 cycles ~f- A- t S Al At is Card 3/5 ACCESSION NR: AT4014055 ENCLOSURE: 02 Fig. 2 - Effect of cycle ze; /I length t and temperature interval A T on internal -1(T) of Cd-Zn friction Q alloys at T = 0. 8 TS. a - 1. 5% Zn, 60 see. (I -AT = 60a, 2- 4 T = 150% -3 -,& T = 200*); G b - 2.95% Zn,--.= 30 sec. -4 T = 100"; (1 -AT = 60"; 2 3 -,4 T = 150*); c - shape of the thermalcycle d - 1. 5%, Zn, AT = 150* (1 30 BeC. 2- -r!= 60 sec; 3 -r=90 see..; 4--r- 120~sea*j 4/6 C *xd 0'5-4~~ Z i~' 'T'i'.' V-~ PFA F~! ACCE SSION NR: AT4014054 ENCLOSURE: 03 Fig. 3 - Relationship Me a 1/01 between internal friction Z~ temperature, number of v cycles and state (A or B) or Cd-Zn alloys. a- shape of the thermal cycle; b -t=30 sec., Ce'v 4 T = 150% T = 0. 8TS (I - A, 1. 5% Zn;.7-- B, 1. 5% Zn; 3 - A, 17.4% Zn; 60 4 -BI 17.4% Zn); o-n=0 (1-A, 1.5%Zn; 10 2-B, 1.5%Zn;3-A, 17.4% Zn; 4 - B. 17.4%-Zn)' z SAS Card MAL'1~3EVAP G.K.; MSTNIKOVj,V.8. I..... .- -1 ~ . Internal friction of cadmium-magnesium alloys. Izv. vys. ucheb. zav.; chern. met. 6 no.11:153-156 163. (MIRA 17:3) 1. Voronezhakiy politekhnicheskly inatitut. MALITSEVA, G.K.; WLGTUKHIN, I.V.; POSTNIKOV, V.S. Effect of temperature on the internal friction of copper alloys. Fiz. met. i metalloved. 16 no.5-.754-759 N 163. (MIRA 17:2) 1. Kemerovskly pedagogicheskiy institut, Voronezhakiy tekhnolo- gicheskiy institut i Voronezhskiy politekhnicheskiy institut. MALITS.EVA, G.K.; K~~TNIKOY.--V-.,S.._ USANOV, V.V. Internal friction in bifiary ordered Alloys'with'.4face-centered cubic,lattice. Fiz. met, i metalloved. 16, $0.2'1'.302-409 A-t' 163.- 0119 16 8) 1. Voronezhakiy politekhnicheskiy institut.::01"ove*' institut. (Alloys-Metallography) (,G,r7ata3.- lattices) (Internal friction) ACCESSTM' NP: AP4009_3391 S101 26/63/016/006/0937/09 39 A11THORSt Postnt%vj V. S.; ZolotukhIn, 1. V. TTq'T.E s The effect of cyclic thermal treatment an the Internal: friction and relative clongAtion of Al-Zn RIloys. SM-RCEs Fizika metallov I metallovedenlye, v. 16, no. 6, 19630 937-939 TOPIC TAGS: Zn-Al alloy,'Intarnil friction, cyclic thermal treatmentp metal elongption, Zn-Al alloy elongation ABSTRACT: The samples studied here consisted of Al with 10; 20, Vj~ 609 e0 and 98% (by weight) of Zn. The initial purity of Al and Zn was 99.99 and 99.97% respective- ly. The alloy ingots were 12 mm long end 6 mm in diameter. They were annealed in a speciRl device designed for measuring the internal friction. Subseauently they were subJected to cvclic thermol treatment, afterrhich the change In their length was determined with a 19R-12 ricroscope. The curves of the relation between internpl friction and temDerature showed a peak, increasing In length with the increase in Zn content from 32 to 98 wt1% Cyclic thermal treatment had almost no effect on the rosition"of the peak in respect to the temperature axis, but it broadened the pepk considerably and increased its height. With the increase in the number of thermal Card 1/2 ACCESSUN NR: AP4009391 cycles the internal friction decreased and renched its adnimum Pt 570 Cycles and then started incransing again. This was true for the samples with 10p 20, 30 and 19SI,- of Zn. The variption in the internrl friction with respect to the number of cycles was different in the samples with 60 and 80% of 2h. The curve of the 60% Alloy h,"d a maximum at about 600 thermocycles, while that of the 80% sample increased grsdually. Orig. art. bass 2 figures. ASSOCIATM's Voronezhskiy politekhnicheskiy institut (Voronezh Folytechnical Institute) SUMMED: l2VaY63 DATE ACQ: O3Fsb64 ENCLt 00' SUB CODEt ML NO FM SOVS 009 OrHER: 000 Card 2/2 FOSTNIKOV, v.S., red. =--tals and allOYS; trm-SP-ct"Ousl [Relaxation P~,enomena in allakh i splavakh; trudy. Relaksatsionnye javleniia v met Pod red. V.S.postnikovao moskval 14etallul-gizdat, 1963. (14IRA 17: 7) 339 P. 1. Vsesoyu',-naya konfererfFO-Ya po relaksalLSIOnIlYm yavl~)niyam j sp:Lavakb. A. Voronezh# 1962. v metallakh POSTNIKOV, V..S.; 14ALITSEVA, G.K.; RAWO, V.I. Temperature dependence of internal friction and the modulus of rigidity of ferromagnetic alloys. Izv. vys, ucheb..zav.; chern. met. 6 no.7tl49-154 163. (K[RA 16:9) 1. Voronezhslriy politekhnicheskiy institut i Kemerovskiy pedagogicheskiy institut. (Ferromagnetism) (Metals, Effect of temperature on) . i.-I 'A MALITSEVA,~,G.K.; POSTNIKOV, V.S.; USANOV, V.V. Internal friction In Gti~,Au and Cu3-Au. Izv. w1s. ucbeeb. zav.; chern. met. 6 no.5:156-161"fO. (MIRA 16.-1.) 1. Voronezhskiy politekhnichaskiy institut i Kemerovskiy pedagogicheskiy institut. (Copper-gold iqlloys-Testing) (Internal friction) POSTNIKOV. T.S. Internal friction in prue metals and allmjm at high tempera- tures. Issl.po zharopr.splav. 4:181-187 159- (14M 13:5) (Friction) (Metals at high temperatures) 3/00/63/9W/00i/069/120 A160101 AUTHORS: Postnikov, V. S-s Zolotuldilm, 1. V.& Gorshkovs 0. As TITLE; Investigation of the mech&Wcal mid thermal fatigue of mtals by the internal friction metjvxl PERIODICAL:' ReferativWy zhurnal, Fizika~. no. 1..' 1963,- 94, abstract 18ftY (In collection: "Talklich. prqobnost' ustallov." N~, AN SM, 1962, 218 -~2~6) TEXT: Investigated was the low-frequenoy internal friction of Cd, Zn, Al, --and Au under mechanical and -thermal fatiguet conditions. It was established that the total amount of defects in polyarystalo; especially strongly ~noreasos during the first 2-103 cyclei, and then a saturation takes place up -to the'failure. Daring the first 2 - 10 cycles, 'an, aocumlation of the defects taken pl 'we, and then defect coagulation processes and other preparational. fracture processes c.o mm e n,c 6,. The amount of defects for the single crystals continuously in- creases up to the failure. The peak of the Internal-fr1otion, which is cham- teristic of.-polycrystalline metals) disappears durina a cyclic load. This Is Card 1/2 8/058/6-VOOO/001/089/120 An investigation of the... A16D/A101 apparently caused by the broadening of'the relaxation time spectrum of sliding along the division boundaries. The thermal cycles also destroy almost OOW*te-. ly the peak of the Internal friction in the polyoryst&llino metal. The latter seems to be caused by a fractionation of tho grains.'. In proportion to an In- crease of the number of the thermal cyclqa, the background of the Internal fr1o- tion increases, passes through the mwdmum and then decreases. Hereby, the background of the internal friction of ,the antal whiah In subj*qted-to a large niAmber of thermal.oycles has-a*smaller magnitude th&n'the background for an an- 'neaae& metal. Mirkin [Abstracter's note:, Complete tianalmion] Card 2/2 -S/123/62/000/024/bOi/bo5 5 AOO6/A1O1 AUTHOR: Postnikov, V. S. TITLE; Internal friction and strength PERIODICAL: Referativnyy zhurnal, Mashinostroyeniye, no. 24,1962, 11 12, Ab- stract'24A68 (In collection: "Tsiklich. prochnost' metallov", Moscow, AN SSSR, 1962, 207 - 217) TEXT: Results are given from investigations of tLe temperature dependence of internal friction for 59 alloys. In ca:;es.when the melting point of the al- loy was below 1,1000C, internal friction wits measured up to the temperatures when the specimen broke down. More refractory alloys were studied at tempera- tures up to 1,000 - 1,100 0C. 'The investig,ations made it possible to establish, a well-defined relation between the internal friction level and strength charac- teristic -s in a 0.55 - 0.85 T. temperature range. In this connection it can be .considered that the internal frictibn level at high temperatures can serve as a peculiar relative characteristic of the material strength in the indicated tem- perature range. It was also established that in this temperature range changes Card 1/2 I rr,,,IK j 025 TO -071/6 Soveshchantye po uutalonLl moballov. 2kid., !Iooooir, 11,"60. Tsilclicho-okaya prochnont' mtallov; n!itorl.,aly vtorogo, rjovr)~7hchaniya -27 1- -1Y '50 C. -al po ustalosti me',;allov, 24 - ~ i, a 11, ~ (CYGlic !?:, Strength; rlaterlala or the Secend Ccafercncc on th(~ Fatl,uc of .1 Izd-vo Metals, hold Uay ?4 - 2-(, 1560) Tioacol W2. 3313 p. Errata ollp Inoorted, V800 co~tleo printed. Reap. Ed.: I. A. OdInC, Corrcup,--ndl,nf-, 111oribcir of thr) Aondelm:j Or Sciences of the USSR; Ed. or 1~kibli3hing Hounot A. H. Chcrnov, Tech. Ed.: A. P. Guceva. PURPOSE. This collection of articlon la inbended for ocientifle research workers and metallurgl~~ta. COVEIIAGE: Tha collection contains p:~p--~va pre8ented and discusnqd at the second conference on fatiguc, of metals, ihich was held at the Institute of Notallurv,-y in Hay 10 ~60. Theve.papc.-rn de-al, with the nature of TabiGue fracture, the mechanism or formation Card 1/0 Cyclic Metal Strength (font SOV/6025 and growth of fatigue cracks, the role of plastic deformlition In fatigue fracture, an accelerated mothod of determining fatigue strength, the plotting of' fntlFqie diagvams, and various fatigue* test methods. War dal;a are preuented on the sensitivity of high-strength stevl to streos concentration, the effect of otreno concentration 6n the criterion of fatigue failure, the erfect of the size factor on the otrent!th of metal under cyclic loadap and reculta or endurance teato of various machine parts. Probleme connected with cyclic metal toughness, Internal.frictlon, and the effect of corrosion media and temperature on the fatigue strength of metals are also discussed. No personalities are mentioned. Each article is accompanied by references, mostly Soviet. TABLE OF CONTENTSt NATURE OF FATIGUE FRACTURE Oding, 1. A. Diffusionless Mechanism of Formation and Growth of a Fatigue Crack Card 2/,P .Cyclic Metal Strength (cont.) SOV/6025 EFFECT OF THE STRESS CONCENTRATION AND THE SIZE FACTOR 011 THE FATIGUE STRENGTH Oding, I. A., and S. Ye. GurevIch. Notch SenaLtivity-or High-Strength Steels Under Cyclic Load Oleynik, It. V., and 1. S. Mezentsev. Effect or Stress Concentration on Characteristics of the Summation of Fatigue Damage Glikman, L. A., and Ye. N. Kostrov. Effect of the Size f _fM_ Factor on Resistance o ',c al-a-To-T-orroBlon Fatigue Markovets, 14. P. Technological Theory of the Size Factor in Fatigue Tests CYCLIC TOUGHNESS AND 32MEWIAL FRICTION Postnikov, V. S. Internal Fl,letion and Tt.-rength 169 177 167 199 207 Cyclic Metal Strength (Cont.) .-SOV16025 --PjQotnikov V S " 1. V. Zolotukhin, and G. A. aorsh74oVq Inv~~~ili~~M ~~echanical and Thermal Fatigue of Metals by the Method of Internal Friction 218 Pochtennyy, Ye. K. Heat Effect in Cyclic Symmetric Loading of Parts 227 EFFECT OF ENVIRONMENT ON THE FATIGUE STRENGTH Karpenko, T. V. Basic Factors In the Investigation of the Effect of Environment oii Fatigue Strength 233 Bykov, V. A., and G. N. Vsevolodov. Corrosion-Fatigue Strength of Cast Brass 238 Chayevskiy, M. I. Effect of Melts of Low-Wltihg- Metals on the Fatigue Strength of Carbon and Chromium- ickel Steels 243 Card 7/9 28062 S/137/6'1/000/004/026/039 A056/A1O1 AUTHOR: Postnikov, V. S. TITLE: Internal friction of plastically deformed metals and alloys at high temperatures PERIODICAL: Referativnyy zhurnal, Metallurglya, no. 4, 1961, 36-37, abstract 4Zh227 ("Belaksats. yavleniya v metallakh i splavakh", M., Metal- lurgizdat, 1960, 264-278) TEXT: The'author studies the temperature dependence of internal friction of plastically deformed samples, from the viewpoint of the atomic theory of metals and alloys. Detailed analysis is given of internal friction due to slip viscosity at the grains boundaries (with a purpose of simplification the author considers the case of identical grains with equal axes for which the slip viscosity at the boundaries is characterized by one relaxation timeC), and internal fridtion.due to the motion of defects in.the stress field. The latter pert.ains to internal friction manifested at high temperatures, since for the given conditions the energy dissipation in the oscillating sample is originated chiefly from the defeat displacements in the stress field. The present reasonirg Card 1/2 24587 8/137/61/oboZoo5/01/b6o ZOT) A006IA106 AUTHORS: Lebedev, R. S.; Postnikov, V. S. TITLE: The effect of plastic deformation on internal friction of iron-base alloys PERIODICAL: Referativnyy zhurnal. Metallurgiya, no. 5, 1961, 32,'abstraot 5Zh243 (V sb. "Relaksats. yavlenlya v metallakh i splavakh", Moscow, Metallurgizdat, 1960, 199-221) TFXr: The low-frequency method of low-amplitude twisting oscillations was used to investigate them effect of case-hardness on internal friction of electro- lytic Fe and Fe-W, Fe-Si, Fe-Ni and Fe-Ti alloys. The measurements were made in a vacuum (---j lo-3mm Hg) on 300 mm long specimens of 0.7 mm in diameter at I cycle oscillation.frequenoy. All the specimens were annealed in a vacuum at 825 0C for 90 minutes. It was established the, int 'ernal friction of plastically deformed non-annealed alloys was high in comparison to that of the same alloys'which were preliminary annealed, and that it strongly depended on the heating rate and the holding time. On the temperature curve of internal friction a peak of internal friction was observed which was shifted luo the side of low temperatures with an Card 1/2 FOM-~., EOV, V. S. Doc Phys-Math 6Qi Interval friction of pure mntrA.- end all6yc tuider hi,-h temperntures." xemerovo, 195~1. (Tomsk Stnto Univ ir-, V, 11. Kuybycl-e~j) 1-61, 178) -2- P C) -T N X 03 1 Is- .t] s4 2 i It I ~l Rip 3 sic 's 0U W.: 8 ~. a :?a I ffi -V tto V ut 14 3 v s - = q, Id t E k I . A i31 A 3 A o S'3 ~Pu *' -1 to to ;: P g -~ u u 1 H 4 Ir OR a - " CH 5 J IV . s -:. R Eli gV38t 4 V IN I tie at -. : -E 38 'A w , I 41. 2 -A u c POSTNIKOT. T.S. Internal friction of pbewl-forza2dehyde plastics at various temperatures. Plast.masay no.11:60-68 160. WU 13;12) (Phenol condensation products) (Plastics-Testing-) Sft,7R/000/011/015/016 10 B013 B054 AUTHOR: TITLE: Internal Friction of Phenol Formaldehyde Plastics at Dif- ferent Temperatures PERIODICAL: Plasticheskiye massy, 1960, No. 11, pp. 60-68 TEXT: The author studied the temperature dependence of internal friction of plastics by the method of small-amplitude, low-frequency oscillations. For this purpose, he developed a "vacuum relaxator" consisting of a,torsion pendulum, a thermostat, and an optical system. Two types of molding materi- als were investigated. on the basis-of novolaks of the type 18, and on the basis of-Resol resins No. 21 and No. 22. The component ratio was changed during experiments (Tables 1 and 2). All experiments were made in air. To examine the effect of air on the degree of internal friction, the samples were subsequently investigated in vacuo. It was found that the character of the curves observed was hardly influenced by evacuation (Pig. 11). It was proved by experiment that the temperature dependence of internal fric- tion changed on gradual transition from pure resin to the finished plastic. Card 1/3 Internal Friction of Phenol Formaldehyde s/191/6o/ooo/o11/015/016 Plastics at Different Temperatures B013/BO54 A peak of internal friction can be observed on the Q (T) curve for hardened resin. In the finished plastic, the number of these peaks increases to four and more. On re-heating, both in air and in vacuo, the peaks dis- appear, and the level of internal friction is considerably reduced. It was shown to be possible to draw qualitative conslusions on the character of temperature dependence.of internal friction of plastics, and on the causes of disappearance of peaks on the Q_1(T) curves on re-heating, with the aid of Maxwell's model and the model of the "linear standard body" ,(Ref. 10). The method suggested is a suitable means of studying relaxation phenomena occurring in plastics under the influence of mechanical and ther- mal effects. For this reason, it can be stated that a systematic investiga- tion of internal friction in plastics with respect to various factors (tem- perature, time, degree of deformation, quality and quantity of fillers, etc.) might supply valuable experimental data to clarify the structure of polymers and'plastics. The author thanks V. I. Rys,Bhentsova~ I. P4 Rotenberg, and P. I. Ageyev, Engineers of the Kemerovskiy zavod "Karbolit" (Kemerovo "Karbolit" Works) and of the filial NII Plastmass (Branch of the Scientific Research Institute of Plastics), for valuable A Card 2/3 88553 Internal Friction of Phenol Formaldehyde S/191/60/000/011/015/0-,6 Plastics at Different Temperatures B013/B054 advice, and the supply of samples. Besides, the author thanks A~ Ya.. Samoylov, I. V. Zolotukhin, and G. A, Gorshkov, collaborators of the Kemerovskiy pedinstitut (Kemerovo Pedagogical Institute), for as- s:Lsting in experiments and compiling graphical data. There are 12 figures, 2 tables, and 10 references: 3 Soviet and 2 Japanese. Card 3/3 PWAKDV, Y.N., inshe High-tesperature cooling of a locomotive internal-combustion engine. Trud7 MIT no.35:108-11? '60. (MM 13:10) (Gas and oil engines--Cooling) /P. R1 0 6 66607 SOV/139-59-3-29/29 AUTHOR: Postnikov, V.S, TITLE: -6n- ~Internal Friction in Metals at High Temperatures PERIODICAL: Izvestiya vysshikh uchebnykh zavedeniy, Fizika, 1959, Nr 37 PP 175-176 (USSR) ABSTRACT: An error was made in one of the author's papers (Ref 1) in discussion of the effec;t of weight of the torsional system on the magnitude of the energy of formation of vacancies; this was correctly pointed out by V.T. Shmatov. This mistake was, however, pointed out by the present author (Postnikov) in the 1959 Nr 2 issue of the present journal. V.T. Shmatov proceeds from pointing out this error to say that "the mechanism suggested for the relationship of internal friction with motion of vacancies is inconsistent since a shearing stress 91 cannot produce ordered motion of vacancies in the direction of @i because Oi is a scalar component of an elastic- stress tensor and consequently such direction does not exist." The author (Postnikov) refutes this criticism by showing that Ya.I. Frenkell (Ref 2), N.S. Fastov (Ref 8) and B.Ya. Pines (Ref 9) also used the idea of directed flow Card 1/3 of defects or atoms under the action of elastic forces. The required gradient of elastic stresses across the ZK 66607 SOV/139-159-3-29/29 On Internal Friction in Metals at High Temperatures sample cross-section was due to non-uniformity in the distribution of stresses (produced by structure defects in polycrystalline metals). The proposed elementary theory of internal friction at high temperatures should be regarded as a first attempt which needs further development. The author (Postnikov) does not say that the hole mechanism of scattering of energy by a vibrating sample at high temperatures is the only possible mechanism. On the contrary, in later papers (Ref 13 and some work in press) it is shown that the hole mechanism does not give a satisfactory quantitative agreement of theory with experiment, especially in the case of alloys. For example, with copper alloyed with 10% of aluminium very high internal friction peak (Q-1 - 1) was found at 920 OC. At FV'1010 OC internal friction falls reaching a value of 9-1 = 0.18. For these reasons the author (Postnikov) considered also, apart from the hole mechanism, a dislocation mechanism. Processes of intersection of Card 2/3 dislocations and of encompassing of obstructions by dislocations etc. (Ref 12) are taken into account since they produce vacancies on a large scale and this ii4creases I \ ~ 0.0000 65731 SOV/139-59-2-30/30 AUTHOR; Postnikov, V.S. TITLE, -f-e-tte-z---t--o--t--h--e ~Ed�tox- PERIODICAL;Izvestiya vysshikh uchebnykh zavedeniyj Fizika-, 1959, Nr 2, P 176 (USSR) ABSTRACT: The author corrects his paper on "The Relationship Between Internal Friction and Creep in Metals at High Temperatures" published in Izvestiya vysshikh uchebnykh zavedeniy5 Fizika, 1958, Nr 6. On p 138 of that paper Eq (7) has to be replaced by U(ai) = Ul - 4,j72mf2a2 02 2E2 i where m is the mass and f is the frequency of vibrations of atoms, a is the mean distance between neighbouring atoms in the direction parallel to tho sample axis and E is the modulus of elasticity. The second term of 'the above equation is numerically equal to the work done in extension, divided by the number of atoms. The text of the above paper between Eq (5) and Eq (7) should be omitted. Card 1/1 n.b. This is a complete translation. sov/lz6-8-2-23/26 AUTHORS: Lebedev, R.S. and Postnikov, V.S. TITLE- Influence of Plas;ic )eformation on Internal Friction of Iron and Iron-nickel Alloy PERIODICAL: Fizika metallov i metallovedeniye, 1959, Vol 8, Nr 2, pp 310 - 314 (USSR) ABSTRACTz The authors describe a oontinuation of their work 'Ref 1) on the influence of plastic deformation on internal friction of iron-base alloys. In the present work, they used their former method and conditions except for a high.er heating rate (60 oc per minute); the error at high temperature has been reduced to about 19'. Results for electrolytic iron reduced by 8, 17, 30, ~7, 70 a-rid 92a,.' and armco-Iron + 40% N! reduced by 20-80% are tabulated (for the Fe-Ni alloy) and shown in Figures 1-5. Some specimenz were annealed at 825 0C for 1.5 hours. Figures 1-4 show internal friction and shear modulus as .functions of temperature for different reductions. Figures 1 and 3 relate to iron and iron-nickel, respec- tively, without annealing; F:L,.,-ures 2 and 3, respectively, Cardl/3 sov~q6_8-~-23/2 g6 Influence of Plastic Deformation on Interna, riction of Iron and Iron-nickel Alloy with annealing. Internal-friction peak values are plotted against degree of reduction for the various tests in Figure 5. The internal-friction curve for iron-nickel has two maximal while the iron-tangsten alloy (Ref 1) has only one. The first maximum disappears almost completely after high-temperature annealing but the second does not. The first is thus due mainly to previous deformation and, as confirmed by activation-energy values (table), is associated with recrystallization; the second maximum is associated with grain-boundary relaxation. The authors suggest that internal-friction values give some indication of high-temperature strength. As before (Ref 1), the activation enargy of internal-friction recovery in iso- thermal soaking was found to be considerably less than that of diffusion or of recrystallization. Although this suggests that recovery is not diffusional, the authors consider that insuf,-:Lcient experimental data are available to discuss a dislocation mechanism (Refs 4-6). Card2/3 Sov/126-8-2-23/26 Influence of Plastic Deformation on Internal Friction of Iron and Iron-nickel Alloy There are 5 figures, I table and 6 references, of which 4 are Soviet, 1 English and 1 German. ASSOCIATION: Kemerovskiy gosudarstvennyy pedagogicheskiy institut (Kemerovo State SUBMITTED: I-larch 6, 1959 Card 3/3 POBI'NIMV, V.S. Relationship between internal friction and creep of metals at high te"eratures. rzv.vya.ucheb.zav.; fiz. no.6:137-144 159. (MUU 12:4) 1. Kemerovskiv pedagogicheskiy Inatitut. (Viscosity) (creep of metals) ACCESSION NR: AR4044012 S/C658/64/000/00'6/E087/E 087 SOURCE: Ref. zh.- Fizika, Abs. 6E664 AUTHOR: Postnikov, V. S.; Sbarshakov, 1. M. Maslennikov, E. M. TITLE: The question of grain-boundary stres a relaxation In. pure metals CITED SOURCE: Sb. Relaksats. yavleniya v met. I splavakh. M., Metallurg- izdat, 1963, 165-170 TOPIC TAGS: grain boundary stress relaxation, stress relaxation,. metal, internal friction TRANSLATION- On 23 pure metals taken in the annealed state there are In- vestigated peaks on the curves of the temperature dependence of internal friction, connected with the viscous behavior, of grain boundaries. For all investigated polycrystalline metals, on the curve of the temperature dependence of internal friction there is a peak caused by the existence of grail broundarieB. The height of the peak depends on the 'amount and fbrm of the impurities; very Card 1/2 ACCESSION NR: AR4044012 pure metals should have a high internal-friction peak. Available data show that the h~-ight of the peak internal-friction peak. Available data show that the height of the peak in the 6ase of Zn and Al depends significantly on the frequency of the oscillations. Furthermore, periodic heating of single-crystal Al and the macrocrystalline alloy of Al with.O.'51o Cu causes the appearance of a peak on the internal -friction temperature curve. This peak appears in that temperature region where there is revealed the, "grain-boundary" peak of in- ternal friction of polycrystalline Al. The--conclusion is drawn that. the, internal.; friction peak on the curve of the temperature dependence of the internal friction of a pure polycrystalmay be caused not only by viscous. slip along the grain boundary but-aliio by some other mechanism. SUB CODE: AS, MM ENCL..- 00 ---Card 2/2 ACCESSION NR:'AR40440qo S/0058/64/000/006/9041/EO41 ..SOURCE: Ref. zh. Fiztka, Abe. 6E308 AUTHOR: Shermergor, Te.D.; Pbstnikov,.V. Ss TITLE: Te 'cation in solids mper&ture "lW CITED SOURCE: Sb. Rel sats. yavleniya v me t -i splavakh. M., Metallurgizdat, 1963, 27-30 01 TOPIC TAGS! absorption coefficient, irreversible process, irreversible process thermodynamics, beat equation, wave propagation, isotropic medium, thermal conductivity, temperature relaxation TRANSLATION: Gives a compari6on of two methods of calculating the absorption co- ;fficient; one is based on thermodynamics of irreversible processes, the other on use of the heat equation. Examines the.propagation of a plane longitudinal wave in an-iinbounded isotropic medium in which thermal conductivity is the only relaxa- tion mechanism. It is found that for high frequencies the wave is isothermall while for low frequencies it in adiabatic; the propagation rates of these waves Card 1/2 ACCESSION Nk: AR4044013 3/0058/64/000/066/AM/Mu SOURCE: Refs zh. Tizlkat Abs. 69669 'AUTHOR: Pbstnikov, Ve Sol'Belyayevi A* MO.' -"'TITLE: The Influence of various factors -as the nature of the temperature dependence of the internal friction of aluminu 'CrM SOURCE: Bb.'Relaksatso Y&Ylenl~a'vxet- I eplavakh. N*. N*tallurgizdat, 19639 164 1 59- I TOPIC TAOS: internal.friction. aluminum !TRANSLATION: Research is conducted using a torsional pendulum an wire samples of. 99.98% pure Al. Analysis of the influence of various factors on the nature of the Itemperature dependence of internal friction shows that with a decrease of the Idiameter of the samples from 5 to 1*5 mm the level of -internal friction is lowered,! and the internal-friction peak in the region of temperatureaft-350*-C shiftk toward lower temperatures. To temperatures of~1500 C a chinge in length of the. samiAes from 200 to 50 mm .(with a constant diameter- of 1 mm) does not Influence, the uwm' tude cif internal friction. For samples with length 20-30 ma in card 1/2 SOV/139-1-58-6-2-2/29 AUTHOR: P0Stnik-QV- -Y-S- TITIE: Connection of Internal Friction vdth Creep in Metals at 11igh Temperatures (S-,q-,yazl vnutrennego tren' iy- s polzuehestlyu metalla pri -r,)rsok:Lkh temperatu-nakh) MIRIODICAL:Izvestiya Vysshikh Ucb.ebnykL) Zavedeniy~ FiZika~ 1958, Nr 6, pp 137-144 (USSR) ABSTRACT: A mathematical analysiE of the movement of defects, principally -vacancies.,, metals leads loo a three-tp-rm equation for iz,-berrnal friction, measure-1 as Q-1. One term of the equaticn coritains --relocity P, 9 another has a faaximum a-f,-, a paiticular temperati,,.xe Tm.. Curves of q-l against temperatlj--,-- for Al, A! + 1~% h1g 'L Fe + 41,7~,', Ni ral-, show mazima, +h9 A' materials at a nc about 2500C and the Fe + 4c/,' Ni at about 5000C. The. f ac..t that internal friction can be expressed in t7erms of creep velocity means that heat ... resisting all~:ys sh-ould have a low internal friotion at, the workin,'s 'I.-Iemperatu-re. Comparison of the curves of Q,-,l against- temperature. for Card 1/2 pure Ni and three Ni alloys (Nich:come, Elzliiioy and SOV/139--58-6-22/29 Connec,5ion of Internal Zmietion wit-h Czeep in Wetals at High Tempej:ature5 Nimonik 80) verifies -this conclusion. There are -2 an Soviet, 2 figuxes and 27 references of which 2- 3 English and 2 German, ASSOCIATION:Kemerovskiy Pedinstitut (Kemerovo Pedagogical Institute) SUBMITTM: 26th June 1958 Card 2/2 80V/126-6-4-20/34 AUTHOR: Postnikov, V.S. TITIE: The Temperature Dependence of the Shear Modulus of Certain Pure Metals, Solid Solutions and k1loys (Temperaturnaya zavisimost' modulya sdviga nekotorykh chistykh metallov, tverdykh rastvorov i splavov) .PBRICDICAL:Fizika Metallov i Metallowdeniye , 1958, Vol 6, Nr 4, pp 706-716 (USSR) ABSTRLCT.- The investigated materials included: (i) Titani=, iron, cobalt, nickel, molybdenum and tungsten (Table 1); (ii) cast and sintered allo s of the "Nimo" type and a cast Nimonic alloy (Table 2 "~ and (iii)-binary solid solutions of Be, B. C5 Til Or, Mn, Fe, Zr, Nb, Mo and W in nickel, prepare(i by a vacuum treatment consisting of heating -the nickel wires in contact with the powdered alloying elements. The temperature dependence of the shear modulus G of these materials was studied by the" inu6hod of low frequency (1 cycle/see) low amplitude torsional vibrations. Since G n it f2 , where 14 le - length of the wire specimen, r - its radius, Card 1/8 1 - moment of inertia of the auxiliary inertia number SOV/126-6 -4- 20/34 The Temperature Dependence of the Shear Modulus of Certain Pure Metals, Solid Solutions and Alloys and f - frequency of the free torsional vibrations of the specimen,- the variation of G was presented in terms of the relative values of f2. The experimental results for pure metals are reproduced graphically on Figs.1, 2, 3 and 4. Graphs 1 and 11 on Fig.1 show the temperature dependence of the shear modulrs (f2/T), and variation of the internal friction of polycrystalline annealed iron. Graphs 111 and IV show the f /T relationship of a single iron crystal. In tOhe 20-44000 temperature interval, f2 of polyerystalline Fe decreases. almost linearly~ The internal frictJ 'on graph shows a ma-,O mu~ at approx 4400C and beginni-ag from tRis temperature f decreases at a much faster rate which changes 2again at about 7700C. The temperature dependence of f of annealed, polyerystalline cobalt is shown in Fig.2 (graph 1 - heating, graph 11 - cooling). The two graphs are similar in character, both being characterised by a0maximum which ocaars at 4500C on Card 2/8 heating and at 320 C oii cooling. A, similar '~hysteresis" O''OV/1 26- 6!74 -20/3;j The Temperature Dependence of the Shear Modulus of Certain Pure hL-tals., Solid Solutions and Alloys effect is observed on the internal.friction. graphs (11 and 111) of this metal. The f2/T graphs for W, Mo and A are shown in Fig.4 (curves 1, 11 and 111 respectively)- In every case -there is a gradual decrease of f 2 with rising -temperature. In the case of nickel., the f2/T relationship has an anomalous character in the 20-3400C temperature interqal (graph 1, Fig.3), being characte;Zised by a ain-imLim at approx 1500C. The value of f4 at this temperature is 15.3% lower than that at room temperature and 11.7% lower than at 3400C. As regarding e solid solutions of various elements in nickel, the fv~ /T graphs of these materials reproduced in Fifo5-10 show that: (i) The anomalous character of the f /T relationship in ure nickel is either reduced or completely eliminated EY the introduction of a soluble alloying element, the affect of Be. C, Ti, Cr and Fe being, in this respect, greater -than that of Ma, Zr, Nb, Mo and W. (ii) The mean temperature Card 3/8 izoefficient of the shear modulus., = 1.dla, of solid U HT L _-O-V/12"44,2p/34 The Temperature Dependence of the Shear Modulus of Cer-Gain -Pare Metals, Solid Solutions and Alloys solutions is lower than that of pure nickel, (iii) Within a wide temperature interval the value of G of solid solutions i.~ considerably higher than that of pure nickel. The V~IT graphs of vavious alloys, reproduced in Fig-5 (curve 3.11 - cast Nimo 20, 1V - sintered Nimo 20, V and V1 - cast and sintered Nimo 28., Vll - cast Nimonic 80) show that the shear modulus depends not only on the composi"ton of the alloy (G of Nimo 28 is higher Wian thal; Ot Nimo 20), but also on the method of its prepa7.atioa- ).t any giwn temperature the -value of G of an alloy prepared by the powder metallurgy method is highei- than that of the same alloy prepared by melting. Theoretical considerations and the re-5ults of the present investigation led the author to the followiDg conclusions: (i) The temperature dependence of G of pure metals can be expressed. by GT = ~o rl + (ke + P flT where o Card 4/8 L_ T + Pr 3 CC the temperature The Temperature Dependen2e of the Shear Modulus of Certain Pure Metals, Solid Solutions and Alloys coefficient of G associated with the thernal expansion of the lattice, OT - tile temperature coefficient of G due to increase of the thermal enerU of the lattice and P. -.the temperature coefficient of G associated with various relaxation processes which occur particularly at temperatures near and abow the recrystallisation tempera-wire of the metal. (Or accounts for approximately 507, of the decrease of G in this tempe5ature region.) (ii) The anomalous character of the f /T relationship observed in the case of Ni is associated with the ferromagnetic properties of this metal. This riew is supported by -the fact that the variation of -P2 J s noz.,raal abo-va 3600C (Curie point of N4 L and that no anomalies are observed if the temperature dependence of f2 is studied in a maguatic saturation fitld (H = 500 Oerst) (Ref ~12). -Akulov and. Konda rsktr (Ref.13) us,--, the concept- of mechano-striction in order to'explain the anomalous temperature dependence of the Yound's modulus E. Dieectly connected wi-th mechano- Card 5/8 strIction is the -vrariaTi,~n of E of ferro-magnetic The Temperature Dependence of the Shear Modulus of Certain Pure Metals, Solid Solutions a.-a(:2. Alloys materials _mder the influence of a magnetic field, or so-calledAE-effe.,_t. The shear modulus is subject to a similar effect, and according to Vonsovs1V and Shur (Ref.15) and Becker and Doerin2; (Ref,22.;', the anomalous temperature variation of E and. G can bo explained in terms of the ZE - and. 41G-effeet-s. -,iii) In -Ghe case of cobalt, the anorialous chai-acter of the f2/T relationship (the presen2e of a may-imula) is associ~eced with the Cop~~Cc , alictropi.- tiar sf oitiation oc'euraving at approximately 430 .. '0 on teaty.ng a:nd at 3GOOG on cooling~ Uv) The fa3t that G of t_-_.e 1"Ji--base alloys is higher? C an rj uhan that of pure _11-i e attributed to the higher resistance to shear by whi-.h the lattice of binary or move complex alloys is ohara,3-~erised. The decrease of the mean temperature coefficient of G observed in the Ni-base alloys (as 3ompayed with pure Ni) can be explained in the following way: The temperature dependenne c--F' G of al-loys can aleo be represented by Card 6/8 GT = G0 1 + %% + PT + Orl T. A.1though the meaning 3OV/126--4-4-20/311 The Temperature Dependence of the Shear Modulus of Cer-tain Pure Metals, Solid Solutions and Alloys Of 006 OT and Or is the same as in the equation for pure metals, the values of these coefficients depend not only on the nature of the alloy components but also on the composition of the alloy. It is kmown that the .M11M present on the internal friction/temperature curve and resulting from the viscous flow along the grain boundaries of the pure metals, either disappears or is replaced by a deflection point on similar curves of alloys. This means that in tale latter case the resistance to shear along the grain boundaries is considerably higher, as a result of which the magnitude of the coefficient'Or is decreased. A further decrease Of Pr of alloys is due to the fact that, owing to the increase of the mean heat of activation, -the process of self--diffusion of atoms in-the !at-tice under the influence of the stress field is slowed down. Although the value Of PT of alloys is not very different from that of pure metals, the fact that (in the absence of solid state transformations) the coefficient of thermal Card 7/8 expansion of alloys is always lower than that of their .30`1/126-6 - 4-20/34 The Temperature Dependence of -the Shear ffiodulus of Certain Pure Metals, Solid Solutions and Alloys components results in that the magnitude of is lower in -alloys than in pure motals. Consequently the value of (Ock+ PT + 00 Of allOYs is 9:1S0 lower than than that of their separate components. There are 10 figures, 3 tables and 22 re'ferences of which 16 are Soviet, 3 English, 1 Italian and 2 German. ASSOCIATION: Kemerovskiy Gosudaratiwnnyy Feda~oglc.heskiy Institut (KemerovD state Pedago" Institute SUBMITTED: 19th November 1956. 6ard 8/8 SOV/126-6-6-17/25 AUTHORS:Samoylova, A. Ya. and Postnikov, V. S, TITLE: Re-Establishment of Internal Friction in Aluminium, Silver and Platinum After Removal of a Load (Vosstanovleniye vnutrennego treniya alyumixii-ya, serebra i platiny posle snyatiya nagruzki) PERIODICAL: Fizika metallov i metallovedeniye. 19531.1 Vol 6. Nr 6, pp 1081-1087 (USSR) ABSTRACT: The authors studied isothermal re-establishment of inter- nal friction in aluminium (99.98%), silver (99,990/6) and platinum (99.8?%) wires of 0.? mm dia and 300 mm length, These wires were extension-deformed by loading them between 15 and 1500 g. The tensions produced in the samples are given in the 2nd col,,mm in the table on p 1081. The tension was applied for 1 hour to aluminium, for 30 minutes to silver and for 15 minutes to platinum, The loads were then removed and measurements of internal friction started within 1 min, Internal friction was de Uermined, using the method of low- frequency (1 c/s) torsional vibrations of small amplitude described by Postnikov (Ref.12). All samples were annealed before the extension loads were applied to them.- The results of measuremer~ts are given in Figs.1-10, Fig.1 shows the Card 1/4 temperature dependence of internal friction and shear modulus SOV/126-6-6-1?/25 Re-Establishment of Internal Friction in Aluminium, Si_.1_-,rer -q-,d Platinum After Removal of a Load of aluminium (Curves I, II), silver (Curves III, IV) and platinum (Curves V, VI). Re-establishment of internal fric-, tion in aluminium is shown in Figs~2-4. The constant; ten-per- atures at whioh this re--e stabl ishment occurred were: room temperature (Fig.2), 4~,00 (Fig-3) r-Llad 8000 (Fig,u"), Re-, establishnip-ril; of internal frict-4on in silver is shown in Fig.6 (at 12000) and Fic- (at 14000), Re -,.E; stab lishme rit of internal fri~;ticn -in platinum is shown in Fi-,-,8 (at 4.500C) and Fig.9 (at 48000, Fi-.10 sives the dependence of inter- nal friction of allumirf-ilim0 (Curve I iras obtained at 20'C, II -- 2150C), silvev (III - 1200C, IV - 1.4000) and platini"11M Card 2/4 SOV/126-6-6-17/25 Re-Establishment of Internal Friction in Alluminian-I Silver and Platinum After Removal of a Load (V - 450OC? VI - 480 0C) on the applied tension in g/mm 2 internal friction was measured two hours after removal of the loads. From the experimental data obtained the authors calculated the values of the heat of activation of re-establishment of internal friction in these three metals. The values of the heat of activation viere found to be 4500, 6400 and 8000 cal/molel respectively. The value for Al was obtained from the curves of Fig.5, which gives the temperature dependence of the relaxation time in the process of re-establishment of internal Card 3/4 SOV/126-6-6-.17/25 Re-Establishment of Internal Friction in Aluminiumi, Silver aria Platinum After Removal of a Load friction, There are 10 figures, 1 table and 22 references, 10 of which are Soviet', 8 English and 4 German, ASSOCIATION: Kemerovskiy gosudarstvennyy pedago i(Illeskly iRstitut (Kemerov., State Pedagogical Instit- SUBUITTED: July 30, 1957. Card 4/4 SOV/137-57-10-20102 Translation from: Referativnyy zhurnal, Metallurgiya, 19 57, Nr 10, p 23 7 (USSR) AUTHOR: Pbstnikov, V.S. TITLE: Temperature Dependence of the Internal Friction of Certain Pure Metals (Temperaturnaya zavisimost' vnutrennego treniya nekotorykh chistykh metallov) PERIODICAL: Uch. zap. Kemerovsk. gos. ped. in-t, 1956, Nr 1, pp 191- 204 ABSTRACT: An investigation is made of changes in internal friction (I) with temperature of Al, Ti, Go. Ni, Cu, Mo, and W annealed at 8000C. The measure of I (Q) is taken to be the logarithmic rate of attenuation of free torque oscillations to Tr (the fre- quency of the free oscillations being -1 cps). The maximum torsional deformation (D) is