SCIENTIFIC ABSTRACT ZHUKOVSKIY, V.B. - ZHUKOVSKIY, V.S.

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December 31, 1967
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SCIENTIFIC ABSTRACT
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HIP 4" ACC NR: AP7003222 SOURCE CODE: UiV66-~-t)7667ii5:Vo-66;rl;52~1183;r I AUTHOR: Sokolov; A. A.; nukove!& V. Ch.; Korovin,# Yu. A.; ORG: Moscow State University (moskovskiy gosudarstVennyy. universitet) TITLE: Stimulated transitions in the radiation from a relativiatlc~electronln an inhomogeneous magnetic field SOURCE: Zh ek6per i teor fiz v. 51; no. 6, 1966~ 1829-1832 TOPIC TAGS: relativistic electron electron radiation, ptithulated emission axial C-L ?C rqOV 7WdA1J1r,1f.W magnetic field, maser theory, ABSTRACT: The authors consider stimulated transitions of relativistic electionsi moving in a constant but inhomogeneous magnetic field. In particle tltir., the r6diation from an electron placed in,an axially symmetrical focusing magnetic field is~Jnyeisti- gated. The probability of the stimulated remission is obtained for an externa elec- tromagnetic wave which is linearly polarized and which propa:aates at a certain angle to the magnetic field direction. From this probabi ty, the*authora determine the power radiated by the electron in the case of ~t trAnbitibna.1nduced by.thp external electromagnetic field at various harmonicsp and thei pcfwdr'of the dipole'; radiation. The region of variation of the harmonics., at which the stimulated emis- sion should prevail over absorption, and is thus of,interest. in maser applications, is determined. Two conditions for emission are formulated1n th4 form of ineqpali- ties relating the different parameters of the problem. Origs arts has: 16 ro=04AS. SUB CODE: 20/ SUBM DATE: 15aui66/ Ono Rul: 001/ oTE .9a: 001 _.L 29671-66... EWT(1)/ETC(f)-----1JP(c-) ---,.AT fACC NR*.- AT6012691 SOME CODE: UR131361651or-OlWI000 00221. AUTHOR: Bo AbLikov A., V.; Brevnov' No N V Zhukovskiyy Go po R10TWAirkwisft M. Ift ORG: SJ qu Uog og At MMI, e -COMMWge omig Dner" MCA* of Atomic Energy I im. I, Vs Kurchatov, Moscow (GosudarstvalhW komitatpo, ispolIzavalyu atomoy energiip Institut atomnoy energii) 'AS" installation TITIZ: Investigation of plasma in the wma: Moscow. T=titut atomnoy energii. Dok1&()y#, noo' 988, 3~65., Issiedova- in1ye p3.aznW v ustanovke AS, 1-22 TOPIC TAGS. plasma research, p*lasma compression, plasms, #jectioln.. plasnold ac: celeration, plasma stability, cyclotron reso nancep. magneti,6 mirror ABSTRACT: The authors describe the "AS" (adiabAie c2Meqaion):: Weirratus: for the I study of a plasma produced by injection of fast ions,, An axially-centered cylin- drical plasmoid is detached from the injector by means of ,pulsed magnetic is accelerated toward a stationary magnetic mirror$ aiA is'~iccqpreaved by &'t increasing magnetic field of mirror configuration. The ihiti&L Ion energy can reach 30 kev. The article contains a descriptioi, of the insUllation (Fig4 ~1) the awd1lary apparatus., and the measurements details*, Measurements were made of the density and potential of the plasma.. the, 31fetimes of the fest ionsp ar4 the Cwd 2/3 L 29671-66 ACC BR: A76o:L2691 Fig. 1. Schematic diagram of "AS installation.-:I - Magnetic leFx,,2 - ch4nnel~ azotite, 4 : titanium evaporators) 5 - chmb'er) 6 7,8,io,11 '": iltationary' mag- 3 1 hetic field coils, 9 - copper screen) 12 - detachment coil)', 13pt - cemprCasion: coils$ 15 - neutral particle detector) 16 - secondary ion energyn pectrum rialyz ens' IT - current receiver.. 18 - rod probe) 19 - palladium leakNalve, onset and development of oscillations at the ion-cyclotron1requen al cy, Theiniti i plasma density was found to be proportional to the injection curireht and amounted to 1016 cirl fast ions at a current of 5 ma. In the absence of Injection- ourrent pulsations, the plasma potential did not exceed +30-40 Y and vae, independent of the injection current or of the neutral-gas pressure* Cyclotron inatabilit~ with an increment time of 20-30 psec developed in the plasma after detachment from the sourse, lasted for about 100 psecp after which it decreased exponentially,,4ippar- ! ently as a result of self-stabilization. The lifetime of the fast ions depended only on the charge exchange with the neutron molecules. The development of pyclo-1 tron instability did not cause additional ion losses. The plasma decayed after compression with a characteristic time of 500 psec. This is several times smaller-,-e.,P~ a beha~vior is!not yet,clear. I ..than the charge exchange timej and the reason for thi The experimental plasma lifetime of the fast ions increased an?ribodmately in prc~- portion to the pressure* Orig. art. bas: U figures and 8 foivulao,, SU3 CQDE 2D/ SUBM11ATE: 00/ 01IMBU: 0051 OTH REF%~~ 005 Card 7~' W.5 1H, HT-fill 113H 11WHR-KI It I. M~i 13 LID LssocTATIONt. 110-uO IVia! It oil 11;3 PM,gr.3 Lill IM11AME11 - R HT 41 ~85018 (/0 Y31 IIYS-1115 3) ~S/040 6qtq2~/01010271033 B01 3XBO61 AUTHORS: Andreyeval N. A.p Grushevskaya, 0. and Zhuk2vi3kiyt V. I.- TITLE:. Some Considerations on the Methods bf Producing Materials With a Smooth Temperature:Dependehob of the Dielec'tricl~ Constant 1A PERIODICAL: Izvestiya Akademii nauk SSSR. Seriyk filti0heskayat ~1 960 9 Vol.. 24, No. 10, pp. 1285 - 1288 TEXT: In order to obtain a smooth temperature dependehoe of the ,dielec- tric constant, the authors looked for an efficient admix'ture totaT102- For this purpose, they chose bismuth. titanium, and irsirconium oxideaiin different ratios and combinations. The system BaTiO -131 Ti 0 was given . ~ 3 : 4 3 12 special attention. Fig.1 shows the temperature dependence of theAielec- tric constants of various samples. It may be seen thiLt; they bec6mie fair- ly smooth by the addition of BaTiO -Bi Ti 0 The maximum (curie po3-Lnt) 3. 4 3 12* characteristic of barium titanate, is, however, not affected. Phenomena Card 1/3 Some Considerations,on the Methods of S/04,8 60/024/0'10/027 3 roducing Materials With..a Smooth 3 2 P Temperature.Dependence of the Dielectric Constant~ of the same quali,tative:character may be also found in':iamplea of the system BaTiO -Bi 0 -ZrO (Fig.2). Fig.3 illustrates th.e temperatu re and. 3 2 3 2 frequency dependences of E and tan 6,for one sample of the system BaTiO -Bi Ti 0 a illustration indicates Thai pres4nee of relaxation 12* Thi 3 4 3 properties. An X-ray analysis performed by V. 0. Prolchvatilov and Ye. I.,Gindin has shown that various compositions of the systems BaTiO -Bi 0 _TiO and BaTiO Bi 0 ZrO P besides :,a phaGe having the 3 2 3 2 3- 2 3-. 2 structure.of barium titanate with changed lattice pa-rameters (not per- fectly cubic), exhibit another phase .which might be held responsible. for the relaxation properties ofthe. material..Solid solutional,which can be formed presumably only in a very small range of'cioncentra4tiong' were not detected in the systems examined. The authors$ studies 14ad'to the conclusion that the materials of the two systems under consideration contain a piezoelectric and a relaxation phase. The vom~osition of the latter has not yet been determined so far. The dielectric constants of several samples showed two maxima. It is assumed that the low-temperature Card 2/3 -1,1,7~600(loq31114'O 107S-) 8/040/60/024/010/030/033 B0131DO63: AUTHORS; Zhukovskiy,-V. 1,, Dorokhova, 1. P.`1 Uromba, N . Ye't 0 Dykman, D. G., Boye, G. V . TITLE: Data of a Thermographic Study of Bariuta Ti.tanad~ , h Certain Admixtures PERIODICAL: Izvestiya Akademii:nauk SSSR. Seriia f1micheskaya, 19609 Vol. 24, No. 10, Pp. 1,294 1295 TEXT: The authors examined the effect of commonly ulled admixtures upon the sintering procese.of barium titanate.- These a4mixtures includie U02, Bi 203 . Ti 02' CaC 03' MgC.03' BaC ~03 ~ et,c. For this ~purpose,, they made use of a complex thermal analyais which4as cond,ucted.Ton an apparatus;of~ the type YKTA-58 (UKTA-58)0.3 Barium ~itanate was :synthenized:at 1$00d. The samples were produced by the conventional ceramic proo see. Thie ther- mogram of barium titanate is shown in.Pig.l. The firot.exothermicleffect appears at 3000C and is related to the burning out of the plasticizer; the second effect occurs at 13000C and is due to the tormination 'of the Card 1/3 Data of a Thermographic Study of Barium S/048M/0201 01010301~33 Titanate With,Certain Admixtures B013/Bo63 production process of barium titanate. The endothelrmic~effect oba'ervable at 8700C may be explained by the conversion of BaCO contained in the 3 material used. on the addition of TO and ZrO two other thermal ef- 2 2P 0 fects are visible in the temperature range 1250+~~.I 2!)Ol C - an endo.thermic effect on heating and an exothermic effect on cooling (Pig.2). This is presumably due to the formation of an eutectic BaTIO, 'Melt withitita- 3 nates of higher acidity andtheir, subsequent crystallization. An X-ray analysisoperformed by Ye. I.-Gindin, of the systemiBdTiO'-ZrO indicated 3, 2 the existence of a solid solution. with a per 'ovskite latti-ceo This: fact is indicative of an excessive.amount of titanate dioxide.. The above- mentioned thermal effects are probably relatedto,~tha presence OfIthe latter. However, the data available do not indicate the compounds that form an eutectic melt. The authors established thiLt a liquid phase exists when sintering a material on the basis of. barium titanate i9ith the addition of Tto and ZrO 2# in the presence of,MgM CaCO 3aCO ~2 3' 3 Card 2/3 ~kCc NRo AiMO30730 SOURCE CODES M/00-5V66/000/0O4/Oi17/0128 AUTHOR.: Kalinin, q., V., 21~91qk ORGt -Dop'artment'of lbeoretioal and Applied Mechanics NI3M (Otdol teoretichdikoy~i prikladnoy makhaniA NIJM) TITISs Conditional stability of motion of an object -trith an automatic control Ovice in some critic'al'aas4s SOURCEi Moscow* Universiteto Vestnike" Seriya fiziki i. kh'imlit' nos 4, 1966s, 117-128 TOPIC TAGSs servomotor, motion stability, aircraft stability ABSTRACTt 'The system of equations forthe motion of an objoot (Aircraft) viih 1 automatic control is given by T + IVIT + kly ~+A=,py,n "M + a Zia first equation in that of the object the motion of uhichAs to;bo regulated;!the second is the equation of the servomotor& Here is the deviation from the,state Card 1/2 I UDCs .531 6391 a 5 ACC NRj AP6030730 prescribed for the system, angle ofthe rudder rotation. is the argument'of the rudder regulation, F(t,J) ) in the characteristics of the seiromotor which determines the rate of readjustment.of steering. The authors cotoider the odso, vhen F(t, is not linear. A linear approximation rosults in a characteristio:oquationo of which the following cases are consider6dt 0 one zero root, 2) one zero~and two imaginary roots, 3) two zero roots, 4) three zero roots* A casD ;Ojr a small:lviaas 'of the servomechanism Is also considered. The general conclusion .1s: that in oiddr to have a stable motion, the nonlinear characteristics of the:servomotor can bo given not only by an equation of an odd order, but also,,under certain conditIA)ns, by.an equation of en order* Origo,art, bass 23 equationse N OjZ SUB C 13 UBK DATBS MAY651. QIM REFs 014 Card 2/2 MONO j. , O-AR6017333 ;-NMOURCE CODE.; UR/0044/66/000/00:L /B046/BO46 ~~a ~d AUTHOR: Zhukovskiy,-, IhTLE: Some instailbility conditions sufIficient for a trivial'[ solution of a sy;siem:of two linear differential ~equations SOURCE: Ref. zh. Matmatika,- Abs. lB205 REF SOURCE: Uch. zap. Orekhovo-Zuyevsk. ped. in-t, v. 22, no. 3, 1964, 36-34 TOPIC TAGS: linear equation, differential equation,-:kuW=Ut"-g1 "9=2" ABISTRACT~ Results obtained in the paper are based on a modification of N.G. Chetayevl s~-ilstabllity theorem The proof of sufficient conditions of instab ~lity has been demonstrated by means of linear forms. V. Toloknov. [Translation of abstract) (KP] SUB.CODE: 12/ .L-Card 1/1 11b UDC; 517. 917 - - - - - - - - - - - - - - - -------- ----- I IJPW L 43131t-66 ENT I ;*#t~'~~P6014168 ~-70N-TKA-f~.Tld-O-ViM SOURCE com: AUTHOR: Zhukovskly, V. 1. ORG: All-UnIon Correspondence DwtItute of Textile and Light MftAusPL0!L(Vsesoyuzn)T zaoehnyy ~wmut ~teks ~Inoy I blennosti) promys TITLE-. Instability and conditional stability in th6 critical case of n verb roots SOURCE: DiffereittaWthyyouravnenlya, v* 1,, no, 12, 1965, 1601-1605. TOPIC TAGS: differential equation system,,'differential eqt3atlon iolution Mor"04); ABSTRACT: The fundamental theorem of motlon instability duet.0 N. Gi. Cheitnyev (TJoh.zap. Kazansk. un-ta, 3btematika,, kn. 9, 98$ vyp. 3, 1938) and the theorein of stability Otte to P. 'A. Kuzlniin (PMM, t. XVM, VYP. 1, 1954) allow the establiolunent of sufflolent conditions for instability and conditional stability In critical ba. cases. The ai -yestigates an antono- mous differential equation system of perturbed motion with it holomorWaright-handisIde, and with a characteristic equation of the linear system in thofirst approximation with n zero roots to which correspond simple elementary denominators of thechameteristIc matrix, :The author derives sufficient Instability conditions (tifforent from those found in the literature (A. A. Shestakcv, DAN SM, 79, No 1, 1951; G. V j Kamenkov, Sb. trudov KAI, No 9, 1939). Card 1/2 5/195/62/003/006/007/61V EOWEW AUTHORSs Vlasovi V#Goo Zhukovs1qy. ',V.M, TITLE: Reductiq'h of uranium trioxide with~ammonia, jPERIODICALt Kinatika i kataliz, V*3, no 4.6, 1962 882-~-886 The kinetics of reductions % investigated in the ;,TEXT: Of U03 wal temperature range 300 to 1k25*C..und0r.l0 to 600 mm KS'partial N1113 pressure a heated aft'~r dr~ying* in high", % a 7 Amorphous U03 (0 .5 g) wa vacuum,in a circulatory apparatus with;'a clontinuous recording-of As weight.losses. The composition of, ep s wash checked,'' I ,d,. producti. 0 4n alr'~And by.Debye-Shereri. by their *ireZd*-6m#OsA:r0ii t U308'' 'at, 0I.C fixed M X-ray anal5#sis. Fdf, a 113 pre3~iure, the.roduction rat ~'decreas6a with decreasing'temperature-~thile the4nduction, period t The dependence of th ratii ok the reaction w an increases. e, partial; NH' is given b 3 P.ressu", Pr4H3 b PN H3 k, CI) P14H3 wh re'- ~k and b are, constants (k e 0,89%/min and Card,1/2. 5/195/62/003/006/007/011 Reduction of uraniuw b 0-00312 mm- 1 fig at-4000c). The apparent activation energy for the process is 45.3 kcal/mole and practicall:~ does 'not depand'.~'_- on the degree of U03^reductio .n..: The authors concludii that,.the-'-^ reduction-islreal-i~md in:the-following stages: '1) adsorption of gaseous NH3'-oh-UO3 surface, 2) docomposition of, adsorbed NH 3#~ N"3 ads -4 NH2ads ~Hads N11 2ads NHads + Ndss. n of U6*~,t U4+ -:~Nfl' Nads + Hads; 3) reduciio 0 ad 02- + H OH + -:e,, OH_ + H -~4 f120ads +,:8; ads adili 41+ ~U6+ + 2e ----r> U 4) rearrangement of crystalline lattice of ithw~ i oxidized phase; .5).dosorption of Pi from the surfacet;. 2Na ds' -4 N N2 gas; desorotiow of H20~ formed during', 2ads -the reduction, The.'slowest stage in this procesaji'stage 5, There are 5 ~figures. ASSOCIATION! Urallskiy politekhnicheakiy institut im. S'4M,Kirova (Ural' Polytechnic Institui~iM_eni*S.M,,K1rov) March 24, ig6i (initially)' SUBMITTED.$, (after revision) Card 2/2 September 11, 1961 '23 1!i 4 ML26/62/014/003/020/022 E039/t420~; AUTHORS: Zhukovskiy, V.M., Vlasov, V.G,,,Lebod-av,,A.G, TITLE, Electrical properties or'the uraniuiai-oxygen system in the ran'ge of composition U03-to U30~11 PERIODICAL: Fizika metallov i metallovedeniyeo,vdi4t no&39 .1962, 475-478 TEXT: The range of uranium-oxygpn c.ampounds:UO2ito U307r investigated by other workers' is.bxtended t0l~cover'U03 to U308'- Electrical conductivity Is measured in the temperature range 25 to 200*C. -Samples are prepared from U03'~by dissociation in a muffle furnace. Spectroscopic measurements.~show~the presence of impurities Na, K, Mn, Fe, Skand Al, the largest component being Na at 3.8 x 10-2%. Debye-Scherrer,X-:ray:analysis indicates that U03 is amorphous while U 08 has.a~hexagonal lattice. Intermediate. 3 compounds show a mixture of the two phases, Eden UO' xhibits 2 37,et Yeak lines of the U308 structure. Samples are form; n o, tablets 14.5 mm in diaMeter and-7 mm thick at~a pressure oC 3000 kg/cm2. Densities after compression arn,3,13,9/cO (for U03) and 3.65 g/cm3 (for U308).. Resistances in the ran'Se 106 to Card 1q,;& s/126/62/6W 03/QgO/022 Electricalproperties, E Oj9/ 7, 011 ohms,are measured using aconstant current megohmmeter'~with -1 an uracy of 2 to 2-00%. Resistances in th~range~lo tW 10 ohm are measured using an ate* bridge at~JODO C/s wit~'!an~ accuracy of better than 5%. Samples are measured tinder vacuum (10-3 to 10-4 mm HS) Values of.the specifie,electrical conductivity x (ohm-lem-1) for U03 and U02~; nd tOOOC 67 at 25 a are given in the table. The temperature dependenc'e' (if the electrical conductivity in given by x A exp(- AF./2kT) -10 where jaE is the activation.energy. Isotherms,df%' x aro'~Si4en I't is shod t~ t and also the, dependence of, 6E on ~compoxitionl.~ A all samples have a negative thermal emf with r4papoct 1o coppdr.~ Both the electrical meAsurements and X-ray analysi.s,,shbw tha~t.- or to greater there is a transition from a state oflow ord for'U03 order for There are 2 figures and 1 table. U308' ASSOCIATIONt Ural'skiy politekhnichoskiy-Anstitu't im.,S.M.Kir~val~ (Ural Polytechnical Institute AM97 i SMAir 'Y). Card :2 /62/01;5/010/001/012 S1080 D204/1)307 -AYMORS %hukovskiy :V.11. and V3.6 0v V.G s 'T I IME .,The offect.OC,alkali:metal earboUates1w.01% the rAte of reduction of,uranium trioxi&v PERIODICAL: Zbu r n a I prikladnoy Ithimii, v.' 35'~ ~noji,!Oi 19 2i 2131-2134 Na-q -Z CO TZXT: Theeffects of analytical pi~rity~iLi,P~,. and K CO- were. observed, on the rated of reduction: of : dm6rpholu 2 Z.) 2 M '3 nt U03 (Specific surface 15,0. /g, dencity:6..5 9 ~Cj -2 - -10-4 'ia.amounta of K In 170 1 ' about 10 Ila M i Al arid d frix4 the c~1~41y~- rwith a dry, 1,116-free mixture of H2 and 142 1 derIve.. tic decompositfon of azmionia. The c4rbonates wdx-al .46d' a 171 roin-&;togeig ~n amounts of 0.2 - 10 mol.5 (W.r. t. ~ U00 I tiara t r trith SU, the oxide, and were preheated for 2 hourjs at 3809C beto'rc the ireduc:- tion. T lie prod Gure of (311,) + -142) was 200 m 11g;:, awl t.he temp~iitture PAIdition slo~r was 4000C in all cases . It was found that carbonat1%. Card 1/2 Card--- 2 Mill SAM= ms m 'AUTHORSt Via mov V.S., Z V TITLEs Iteductign 0,C uramium trloXidla by a, PUZODICAL: Kinetika L katalim, 4i TEXTI ~ r, ~-I-- Thie wor C,. a a: Coll ftwi tion at kiddtI16, altudles- of the Aim antarplimtv U V radtidtiam qf U03 with various gasas~ 03 itl the surface area aC 19 uj% and density (~r 6.5 gletzt? %-ao raduaad with a mixt,tre Of N2 a" U2 reumlt"L& from the reductiam of W13 over Ni at 930-C. Full. tranmition from UO> to U01,1 wal; colUaidetred as 100% reduction. The redixctiort was studied b,styo,(Ion 30-0 and 500% at a pressure or P 31i?-.N , 200 mm Hg, mad at 425"C, vith 2 preasures ranging Crom 25 to 6013 mm HE,# The rato of reduatlon~ increased rapidly ic:Lth tomporature, nO indU0t40,n p0t'iads beillig noticed.. The effoct of pralsstu*o an the reduotion v~r. t vv f. a expressed by v a kpH pj~ boing the partial, prtils'amr-ov of hydrogen. The vatluai be mrs m?P12-oxiarately C.111,15. Tho roductian is thereCore iadopend-vat OC M2 uhich 4kctm only a a a diluent. The pracesm takes place In the follmrimjr tita.gesl Card 1/2 Reduction or urdlitum E077,/EI43(1 1) U03 -) U02'.92 reducticiu ratm constdint; Z) an auteentalytic pro'ceslis IJkI UO '44H UO 141,- 0 2.92 aaorph. 2; C'm a 2.67 CrYgil 11 &AIS 3) UO H UO H 0. 2.55 cryst. * 2 gas 2.125 2 get a 4) UO 2-55 U02+x U02 The first atage takes ploce Ln the pVesen(llm Of two solid phaten and the second. in the presence of oine itolid pimse or rhallaing com-Ooffitim with the roduction rate fallinig continuounsly. Tl,.v, mpparent activation anergiam for the various stagea of j,*dkttA3cm vary er-cam 26.5 to 31.7 kcal/mole. In jranarail, the rediuctimi with N2 + H2 ocemrrad more easiLy and to a futleir sxtent 11-haml A1,1'.111 qtth NH3. There are 4 figure4i, ASSOCIATIONs Uralltslciy poIiIP4chn;,cheaItiy institut 1.113. S.M.Ktrava', (Ural POlYtOO.IhILiC TVkOJtit%'t0 11IM111. 11.)1.311rCIVI SUBMITTED: May 1,;, 1961 (initiflIly) Card 2/2 Septomber 26, 1.961 (aftor rayls:Lon) AUTHORS: Zhukovskiy, VVM.-, Tkaicheinko, Ye.V. Vlavov,, VA. TXTLE.- On the quastion~ of~:pbwtsq -conversioil: in PEAIODICAL: Fiiika: metal 110V~, 1.1 tie ta llovad4raylo, 11 15,1 visa.22, 1~63, :77 210-214 TE.' o,. contra d Let ~46~k 4'hc.4411 ~`Ori ~ith!t t1s h is ions In -the tl'- 0 daysteva Cori thit and range U02- U02.25 is examined. The dependonce of tLte density anfl parameters of.the cubic lattice on the. compogition ot the raoli.V phase formed in reduced U4.09.,i%,rhen decomposed by ammwida and $6 ,id carbon is invostigated. With increase in quantity of introduced oxygen the density of the oxide is increased and the lattllce parameter decreased. When the oxygdn content of t,tia omide is changed it is necessary to alter the charge on some of tho urartiuai ions in order'to maintain electrical neutrality. In particulAr in U02 uranium is found only in the torm of Uk+ ionm (ac.-cordin$, to the authors' data), the lattice parameter is 5-417 X and the donsit 'y is 10 7 j1cm3. In the ease of U~'39 Yhich has a lattloo pararito-tov, of 5.44 and a density ot'll.4 S/I;m3'0 it is noodinsairly to altai the Card 1/2 F S /.19 -rddt~bos th u a ~90 2TO -On, e, q e ti46n. of,phas 3 :1 + n soma of the.. utartiuaA -ii6tid frbui ~U ~:~to~ V, harge. o it substitution Q f, -some: 4+ ~ ~ - * , 5+ i-I ons ~b~r~ the I sriaillei~ U. ions Yt -1ea d- to, a decrease in: the 14t:tiii~b pa'x~aaetor.:for. U40 ,the introduction ~of m re'ioxyzen.: j th 6 radil 1 V5 n 0 a 41 u6i ions are 1.05, 0,91 and 0.79 X respectively) . 0onsitios maa,#~rO4 -experimentally compare well with thosie detersaine.4 f i:.mii X - ra y diffraction arutlysis. The resultis are in agreeiviani. with the statement that the phase of U02+x has a cubic lattic-4L~ at' the fluorite type with disordered introduction of surplus oxygen wid four atoms of uranium in the elemoxxtar.y call. There are is fiAiAreal. ASSOCIATION: Urallskiy palitelchticheskiy insti'ttM ilrl~ 8*J1.X r0 Wral Polytechn:;icia ~ III f T:ztitute imeni S.M.3:irov) I t 11M 114", .~ ..... . - - - "I, - I I I a 11 -1! 1; 11 11 11, 1 11 It ['~ .11 1 1 1 1 ~ - , I, -. 1 '1 , ~ . , . It! I 1 11 [1 1.1 ... 4.: 1. 1". - I - . I. . W w 1 1 4 1--., .1 A w 0 w IF v I ! f" I - .11' 1. .1 .6 OTT# Mr-Ir? 147-A"a tog jqpj.~) .. I PRO A'4 Ism jos!:fi do A dd; 6oft 1 bet a dwpAtlayi QM M, 11"Nu .00 -00 Sao A e . see See. WOO goo wo 0 L/ =- a $*am M., d g m wee .1 U a** .6. G.. l sa O 0 owe el: 0 00 41 0 6~0 a MM .42 o " " 0 0:* .00900,00 00000.0 o 02;0 0'0~0 0 I 4 IEJ I. .......... 6M MME.M. A. MY i I ..H.I.M., . ..... *foil $1 ft a 11 m I.- it SLAO #Pa a 10 0 ~.w 14, v is A. 11 v k k :64 8-9-6-k-1 1A-A-4 --J- 4.A 1, - 1. ~y A-L-L-m Of.. rA,111. JZ p-1 Jill A- C.. v 00 4 .00 00: so nowspawd* Ot 1~ftafds dk"~ '00 and walor usdef tho too" af==UOO. 00 ""'1, 11,46 All Tf- illy 'f Ilf Ird. Iji- % 0%t 7go* 40 Uo goo ,go 0-4 goo goo 400 Me 0 a0 L too big 0 Va! .... ... ... ltj/ vea.~ I all. ;.t u 4, IV ty (W f(malcm Knu six 000, '00000 0 04 0 0 * 0 0 00 * 0 0 0 *10 0 0 * a f) 9A) 00 0 0.0 0 0 0 0010 0 0 So 0 0 0 0 00 00 0 # .0 0$01,0 0 o 0 4. 11, 0 0 0 0 a 0 0 it t v ill.- art id, !I a is a lot 044. It EMS .0. Sz-OllullwA $0 z 1940, ;1 00 a ' 130 fm m Akw z;;~ The jfwwn. W; tb* hydr*Sh to 6q. Wt ~4 Ao -,1k k wy* 404" the Im %WWO it 11AV I I rac 0804" rouaw Obw "10 004 wow 1w, 1,! " *Nftt cc th"a 1"S WON tMew I. 09,3 400 see _ ee 00 W s 00 sodl ago as* AIG-ILA 04tALLIMMAL LMOA I "ISOO 016 aR lq' "tax M A I ' S too K Aw )a al; IV to It " of it A h UP:a Ame OL: : 0 So 0 So 0' 00 0' Q im p0 : 1 e ::o So i 0:& In 000 * 0 0 .0 M Z A a , . -0. 4..0 0.0-0 00 0 0 A 0:0. 0. 0 0.0 v 0 o v g4) *41 ID e9.0*0 . 0 A em ; - 094 .00 00 go l 0 ee Ab*4y 7%traW *dfti WA. ftd~ dynawks. liftI ~ Tn-billod as 04F ae .3 at Arrm d F"" V, $?It, . IL 1 ~W lop, ' -To s 004 AAA J`* 0 tA jt 'J. F AS)OLA IATALLWWAL Ul"At"I cimjvvAfwl::~:i~ V4 a are;: 04 8 c Vv 1 f !I f fF 3 al ff 2 j!:fL 1 : .............. Call. 1164 AY55iOW C 6 0 0 CA 3 BOOK Axithor: ZHUKOVSKIY, V.S. ftn' Titli--.--TEM=AL7THERMODYfl~AkiS (3rd ed Io Transliterated Title: Tekhnieheskaya Term6dinamiM. Publishing Data Originating Agencyi. None Publishing House: State Publishing,House 'of Teehlifcal-ThboreticAl Liter~iureo; 0! 'Datei. 1952 No. pp.: 408 (text).and 29 tables No 4! cc i ple a: l5jOO1 Editorial Staff Teohniciil Mitor: None~ Editor; None. r 14)praio" None i Editor-in-Chief: None* Text Data Ooverage: -The third revised edition.is supplemented by he following newl, -subjects-, tendency of isolated s7;stems Ao this; Ma~6:'of eqaili~wii~ft; differential thermodynazie equatione ail q poteatial~~ O~Oles Of*gas turbine-and refrigerating initallatlonh* 1i the ~ chapt4is on technical application'of:thermod ynamics. only eseon~#1, in given and details are: referred :to --The main object -of ithe -is prlxwuy to i*ineg q. clear understanding ~Adq itio he. ~9' ofthe basic subject of, the problem ~ under coniq rr n' t - Pecific methods of its solution,:: and interrelation ok~ ~th-i O*en met-ha, of scieittific.:analysis with otlwr,metfiods&~: Purpose: A textbook for students in institutions of higher Uaining and 6, t~ermo- chemical in titut ons. 1/2 U- O-VS7, Fl- AID P 1256 Subject USSR/tngineering Card 1/1 Pub. 110-a 17AT ,Authors Zhukovskiy, V. S., Doc. of Tech. Sci.i., et~ al. Title Deych, M. Ye,, Technical Gas Dynamics. Gosenergoizdat): 1953- (Revi w) Periodical Teploenergetika, 1 62-64, Ja. 1955 Abstract The book of,M. Ye. Dey~ch.outlines the principles of gas , dynamics of the sections of turbines between the inlets: and outlet valve through which steam passes~. It tou;chtp's also upon the theory of turbines. It! is Intended as a: textbook for students. Institution None Submitted No date AID P 1333 Subject USSR/Engineering Card 1/1 Pub. 110-a 15/19 Authors Kazavchinskiy, Ya. Z., Kand. of Tech. Sci. and Martynovski-y., V. S.,, Doc. of Tech. Set, Title Zhukovskiy, V. S., Engineering Thermoclynamics.(Review) Periodical Teploenergetika, 2, 5T-59s F 1955 Abstract The textbook on engineering thermodynamics of, Zhukovskiy, V. S., 3 rd.: ed., revided, published -by Gostekhizdat in 1952, iolreviewed. Institution None Submitted No date I ?I , , III 1- -11":P1 1 --- -------------- ZHUMSKIT -- ToSe-.-prof,-- rat senzent; --KNCM --red. ;-BOH1SWW1T, ~I-Xq- --- re'd.;Z&M~MMp A.A., takhn. reds [Problems of aerodynamies.arict hea~b transmission in boiler farnace processes] Voprosy derodinamiki i toploperedaefil v 6tallao- t6ocbm7kh protseseakht abornik statei, goakrao'Goo.' anere. izd- vo, 1958* 329 P. (HIU lltltO) (3krwass--Mrodymmics) (Heat-Tmnsmieffion) GMSOVA, Tekaterina Aleksandroyna; ZEUKOVSKIY, Mikhail Isaakovich; ZATADOVSKIY, Anatoliy Klkhaylovich,, ZYSIRA,-MCLOZM, Larjea Mikhaylovna; SMRI, likolay Akimovich; TYRY=IJr, Ve'Isvolod Georgiyovich; ZMOVMY, V.S.4 prof., doktor tekhn.wiuk* red.; KWATMADZE, B. # prof,,`-'d'6ktbr tekhn.nauk, red,;, ZHITNIXOVA, O.B., teklm.red, [Aerodynamic improvement of bladed apparatus!,of atealm and gas: turbines] Aerodin'amichookoe sovershenstvovanie lopatochaykh~, apparatov parovykh i gazovykh turbin. Pod red. 7,8.23mkovskogo I S.S.Kutateladze. Moskva, Gos*energ.izd-vo, 19,50. 340 p. (HIRA 13:7) (Steam turbines) (Gas turbines) S/170/62/0'05/-3q7/005/010 B10,1 /3112 k~,.TIMR: S. T ITLE isothermal flow of g-,as throug1h pire-i FZ7~ IOD ICAL; Inzhencrno-fizicheakiy zhurnal v- 5, no. 1962 45-51 TZXT' The h:r2othasis of L. A. Zalmanzon (Protochnyye ej'&-qnty ikh priborov kontrolya.i upravleniya - Floivo ments ofi pnevma'ichesk cle pneumatic control instruments, Izd. AN sssia, 1961) and ~ SISM . Thristianovich et al. 'Prikladraya gazovaya dinamika - Ap,)Ved Gas dyna, 71 cas in a ,j mics,. 1940-that t-lie .11sach number of an isothermal flD Of! pi.ie can approach unity, and some conclusiond"I(lerived therefrom, are .4: V reiuted. Under conditions of convective hea'k; transfer 'n ii3othermal flo's ~ izA oe gas in-a pipe can occur in a completely determinea relationship of number 11 at the input of the pipe and M'ach number it at., the out ,:a c h u Pt: 1 2 t- 4+(2-r)11)/(4+r~-'i), where r is the reduction factor,, and " % 1 2 1 - Ps In + ( P1 WM 2 A P, Card 1/2 /170/62/005/007/005/6101 Isothermal flow of gas tbrough pipes B'104/3j12 As this relationship is close to unity, the~interval of possible 11-iach. numbers that fulfill this relation becomes extremely narrow. Hence, an! isothermal flow of gas in a pipe can be nbtained only-if1the pr4agure drop is very small. There is 1 figure. ASSOCIATION: Vysaheyo voyenno-morskoye inzhenornoye uchilishche imeni P. E.-Dzerzhinako.-of g. Leningrad (Higher Naval ~3ngin'eering: School imeni F. E. Dzerzhinskiy, Leningrad) SUM' 'D: October 25, JTT! -61 Card 2/2 1. Vaesoyumnyy zaochnyy onergeticheakiy inatit-ut. 9-L~ , , T "Ijw~4 -1 , H- " , ril, I r .~ In IM I - . J I " I , , ! - mt I., !1.[. 1. ". ~ I 1! 11 ~ I ;~ !) :P, 1, ! ~ 'j ~3 . I - I . -i ~ 1 .2 Fit ;,F III;. A.A If I I; T~- AO~)9,(A U: C6 AUM0113; ZhukovskAy, V.S., Hatnikovich, K. 1. (Leniugrud) TITLE: He&t wd masex trarnsfer in air codlers wit2i spirthl-l'iiowd tubas SOURCE: Teplo- i massoperenos. t. 2: Teplo- i wmssapeTonas pri fazovytdi i khImichealkildi prevrmshcheniyaldi. Ed. by A.V. LOto% arxi. B.M. &W- skiy. Mins%, jzd-voAUI 391M, 1962. a06 - 214 TF..Vr z With respect to the 'aoeTfi(Aetut cif heat tvatisfew frotA th,,~ air !iA spiral-finned tubes produced by rolling-on di ffer only 14.1 ttdo f T ov. (-j rcular- -ribbed tubes with wound-on spirale mr:er ~he conditions of jrooc ccntict of the ribs with the supporting surface. Stability of the hea.t conuftict ijiclr.-~endently of the operating conditions is &u &dvantago of rAie rolltng-ou rwthad. The coef- ficient of heat transfer can be ca-lexilated from the dependenaes Nu im,7;0*077. tdO*7! T~ tUIL-voi=6 _._~.:,::.developied by the authors-~ anti 111if ture contents up to 10% should be deteridned on tbe assumptbon or it a1ridlarity ----------- 7.7 .177-7. 77 7 41 I I Mill Heat and masa transfer in air cooleva .... _t Idh from MY oq110:11t,r:1 Wti-L) o Nu, of the partial preissitre and tomp ratu" rie i where NuD is the Plusualt diffusion ariterlon. 7he hydmu1i(!: re-ifit"tarl-.0 of Qpt- ral-finned tubes at which moistura conden-,ration ocours Is in ox xt 1:_s C,f -he nl~- sis"nce uf circul.ar-fluied tubas in. di7 air, and In appraxlimtt 11 - ' _e o.417 Eu n Re- where n' is the number, of longitudinal rows of tubes in the d:1ivA;1s)n of flovi. The entrainment of miisture at velocitier:, of flow exceltiding 145 :V~mo is extrn*m- ly great and attains 60,15" of 'hat candensed in the cooltyr. In Ud,1 oase, partj- cularly efficient viater separator-:-, should be uaed which, la m-did t1on '~.o a ocale- -up of the device, results In a ftart1m,-r Increane of the roaial-A: cats whir.~h wet-q contviderable a-*z;o wi~hoi~t 'U-As faraz Lnterienlng. An approprIal, ~Appar limit of velocity is 10 - 12 a/sec idiich ia usually rehoonimDrided and &L wi loti a sci' paraLl.on t'0 "'r- - -,0% of the s-appl-led rnis-~-Lire Is obtal--iea the mo. t i-iin:110 separa- -~,bes ,,r.. '. s iti-, riba sho-ji a ro-ug~) in-~ernal surfa.,cirj 11. t,'h ;ff Ie r-a ti ri~lj f !a% depress'lan.5 &rid pro.)ef3tlona r,_5k:imb.L1.-4T, 1~he -,hraad o' ii, t;ci'~ -4. D-Le -n rsi~ah an rouFPLrjeqs", Lne oom_ffIclianT, of ne&T transf,ir, frrr ~111!a !alter n1do is twice th&t calculated from the current dependonees. This af-ert !E partle~ij- Card 2/3 US !"ME. ~MFM 1:S' I I S/8 5Q eA.10 2- /M 0/02 V029 Heat and mans trmnst'er !n air coolers .... A05-11/lk 12-6 larly us-aful far finned Vibes. V.Mo Anturlyev, G.S. SebmsXly, mid lAw Too- trallnyy InstItut tokhnologil nmahlriastroyoniya (Oantvttl InAltitt ".mchra'.ovzr of MaclUne Dullding) (Ts3'L-L7R-"'h) are ii;entioned. There ar-P It luld I t-P ble. . . : . . . I T I !. I I , :1 1 ~; . 's - - - --- -- -- .. - . - - - - -1 OW." I I I I 1311M, i . : ; . . I I . VIN. i . :i I I I 1111 11 ~; I Mi ! 1;,[: 11 . , AUTHOR: Zhukovskiy, V.S. (Moscow). 24-7-19/28 TITLE: Distribution of stresses in notched rods during elastic' plastic deformation. (Rappredeleniye napryazheni-y v nadrezannZ(kh sterzhnyakh pri uprugo-plast.icheskom deformirovanii). PERIODICAL:"Izvesti.va Akademii Nauk,Otdeleniye Tekhaicheskikh Nauk". (Bulletin of the Ac.Sc., Technical Sciences,Section)t. 1957, NO.7, PP-132-136 (U.S.S.R.) ABSTRACT: Solutions of the problem, published b ]Jzhik, G-V-.~Ms Grubin, A.N. and Likhachev, Yu. 1. (2) 6ynd Likhachev, Yuj.(3) of the distribution of the stress inside the narrow cross section of a deeply notched.specimen under tensile Stress in the case,of elastic-plastic deformation are approximate and the importance of a number of the assumptions made is not quite clear. The results published in this paper aimed at clarifying some of the problems involved. Due to the' existing analogy between the problems of plane and axis-. symmetrical deformation, it is possible~to verify certain conceptions relating to the elastic-plastio deformation deri-ved by means of the axi4-symmetrical problem by 1/3 experimental results obtained on plane specimens. In a series of experiments the deformations were measured after Distribution of stresses iyotched rods during elastic- plastic deformation. (Cont. 21~1-19/28 successive loading steps at various points z the-axis BB, FiS.1 (axis connecting the roots of the,notches of the front surface of the specimens subjected to tensile-stresses in a test machine. The shape and the dimensions of the notches were,the same as those used by Uzhik (1). In the graph,, Fig.1, the stress distribution in the narrow cross section of a deeply notched tensile specimen isicompared for,axis- symmetrical deformation and~for plane deformation. Fig.21 gives the dependence on the~specimen thickness of theAnerease of the curvature radius, of.the axial deformation and:the stresses at the apex of the notch at the instant preceding failure. Pig-3 gives the dependence of.the axial deformation, the stresses and curvature radii relations at the apex of the notch of a thick specimen on the nominal stress in the ~ narrow cross section. Fig.4 gives the stress distribution in the case of plane deformation calculated.by various.methods; Fi&.5 gives calculated values of the stress distribution'for the case of axis-symetrical defotmatioft:, usbig the same, solutions as were used to determine thecurves of Fig.14., 2/3 The available results are compared. For the case of plane deformation the results are considered which were obtained Distribution. of stresses in notched rods'during elastic- plastic deformation. (Cont.) 0/28 IrSt24-J-19 n by,B. P. Kishkin in his dissertation res :e neentration. in the case of plane deformation and failure of a beam~with deep notches", who used the theory of small elastic-plastie deformations for determining the stress state of a tensile stressed steel rod under plane deformation with a specimen configuration similar to that shown in Fig.1, P.132; the stress epures in the narrow cross section cbtained by this author for the fracturing load are plotted in Fig.4. For. the axis-symmetrical deformation the results of Likhachev, Yu. 1. (2 and 3) are discussed, who gave an approximate solution and considered the large plastic,deformationsoand the increase in the curvature radiusat the apex of the notch; tho stress epures obtained by him~are plotted in Fig-5 and relate to cylindrical steel speciinens with a,deep notch of hyperbolic profile subjected to:tensile stresses. Grubin, A.N. and Likhachev, Yu.I. (2) did not take adequately into consideration the change in the curvature. radius at the apex of the notch at the in'stant of beginning of failure. The author thanks G. V. Uzhik for his advice 3/3 in carrying out the here described work.There are 5 figures and 9 references, all of which are 61aviot SUBMITTED: November P-81 19566 AVAII&BLE: AUTHOR: Zhukovskiy, V. S. (Moscow) SOV/24-58-5-21/31' TITLE: -0 -tE6,,c-ourrxcxenv-W-Mtrengthening and tha Character of Propagation of Plastic Zones in Notched Bars (0 koeffits:bente usileniya'i kharaktere rasprostraneniya plasticheskikh zon v nadrezaimykh sterzhnyalch) PERIODICAL: IzveBtiya Akademii Nauk;SSBR, Otdeleniye Tekhnich6skikh Nauk, 1958, Ir 5t pp 116-120 (USSR) ABSTRACT: The coefficient of strenthening f of a notched bar is the ratio PiP,, i.e. the ratio of the load at whi.6h. a plastic defo at ons in the weakened cross..section ate for the first time larger than the elastio~def6rm*ationsl-,-bo~-the ,smooth bar, yield point of a, the cross section of which~is equivalent to the narrow cross seetion:,of the notch6d bar. Study of this coefficient is of.defibite inter6st~' s'ince it provides additional possibilitieB.oi verifying, experimentally certain assumptions of-the theory ofj,', plasticity. -Uzhik (Ref 2).has shown that9' due to three- dimensional non-uniform tension which ?~in the case of a~ deep notch, takes place along the entire narTow cross section of the cylindrical or plane deformed bar the Card 1/4 development of plastic deformation which Btarts at the 807/24-158-5-21/31 On the Coefficient of Strengthening and the Ch6racter of Propagation of Plastic Zones in Notched Bars apex of the notch and extends towardsthe narrow cross section will be braked, whereby in the.ci".e of a sufficiently sharp notch the na row.'cross s-ection will be subjected to elastic-plabvic deformation until the ' ~ specimen fails. The deformation of tensile stressed bars in the case of.a bilateral notch,~ Fig'.1. was studied by Southwell and Allen (Ref 3) within,the framework of . the plane problem by means of the relaxation- (,numerical) method andl in the same way as in thelother quoted~ theoretical work, they did not take into consideration work hardening. Hill (Ref 5) assumes t1tat plastics deformation develops rightacross the narrow cross section of the bar,and this prevents formation of an elastic core; according to the formula of Hill the r~espedtive numercial values are calculated and entered-in a table, p.ll~'in . which theoretical results are also given of Southwell and Allen (Ref 3), Jacobs (Ref,4) and-Hill (Refs 5,6). The greatest divergence between the f values'pertain to plane deformation which is also confirmed by the data of Card 2/4 Jacobs; for the plane stress state when there is either. 80V/.'?4-58-5-2l/3l On the Coefficient of Strengthening and the Character of Pr6pagation of Plastic Zones in Notched Bars no elastic core at all or the elastic core is very small (Fig 2), the divergence in the f val-~es is small. As the basic assumptionwhich justified them character of the propagation of the plastic zone, Hill considers the requirement that the notch should be sufficiently deep; this contradicts the results obtained by Jacobs (Ref.4) according to which the character of ~he deformationidoes not change right up.to values of b/2a -~ 8. There is~alio a contradiction between the results ot:Hill.and the data' of Green (Ref 8). Equally, available 93q.,erimental data~, do not confirm the views expressed by Hill.;.it can be assumed that the views of Hill are correct for certain types of notchesi for instance, forvery obtuse-angled notches. In the latter part of -the p&per the author; deals with the approximate nature of producing the plane' state of deformation experimentally and refers the reader to the Candidate Dissertation of B. P. Kishkin I'Stres~s Concentration in the Case of Plane Deformation and Failure in a Beam with Deep Notches". furthbrmore, he Card 3/4 gives experimental results obtained for 70 mm. long notch'e.d Oil the Coefficient of Strengthening and the Character of Propagation of Plastic Zones in Notched Bars specimens of various thicknesses with'varl6us character~- istics as enumerated on p 118. The experimental results, graphed in Fig 5, show that for very thick:specimenB'.the transverse contraction is small partielularly in the, case of sharp notches which contradicts E0 results of Lee (Ref 11). The experimentally obtained-values of~. f are shifted towards lower values as colapared -to those calculated by means of the.Hill formula~'a; the greateA divergence is obtained for specimens with a sharp notch, of considerable depth. It,was fovnd that the sharpnoss'~ of the notch did not affect appreciably the-values of. f and this is in a reeme .nt with the results of Allen and Southwell (Ref 35. For thin apscimens the data graphed. in Fig 5 are in agreement with the data of Siebel and Hosang (Ref 19). There are 5 figureel 1 table and 19 references, 11 of which are Soviet,,? 19nglish, I German. SUBMITTED: December 2, 1957 Card 4/4 Y PHASE I BOOK EXPLOITATION SOT/2566 J. Akademiya nauk SSSR. Institut mashinovedeniya Problemy prochnosti v mashinostroyenii, vyp.,2(Problemil of Strength''In Moscow, Izd-vo Machinery Design, No. 2) AN SSSR, 1959. 97 pe- Errata slip inserted. 3,000 copies printed. Resp. Ed.: N.I. Prigorovskiyt Doctor of Technical! sciences Profes4* sor; Ed. of Publishing House: V. M. Klennikov; Tech* Edt: O:;*M* Gus1kova. PURPOSE: This collection of articles is Intended for scientificj research workers, engineers, and designers. COVERAGE: This collection of articles,deals with stress concentra-1 tions. The topics.discussed Include stress concentrations in., holes of equal and unequal ratio, stress and strain distribution In flat notched bars, residual stresses during heat treatment, and stress distribution in a wide strip with a hole,near the edged No personalities are mentioned. References follow each articlee. Card 1/4 Problems of Strength (Cont.) ")OV/2566 TABLE OF CONTENTS: Preface Vagapov, R.D.0 0.1. Shishorina,.and L.A. Khripind. Method of a Superposition of Kiiown Contour Functions for Evaluation of Stress Concentration for Several Holes of Equal Radii (Plane Symmetrical Problems) 5 Vagapovp R.D., 0.1. Shishorina, and L.A. Khripiria. Approxi- mWVe'-E-v~-1-ua-Elon of Stress Concentration at Mutual, Effiect of Holes of Unequal Radii ~31 The fore-going articles are discussions of investigations made by the author at the Laboratory of Dynamic Strength of Machine Parts, Institute of Mechanical Engineering, Academy of Sciences, USSR. In these articles the authors develop a method of linear superposition of known exact.solutions for stress concentrations for each individual hole with aDproxi.. mate stress concentration due to mutual effect of neighboring holes. An experimental check showed full agreement with the approximate analytical solution. Card 214 Problems of Strength (Cont.) SOV12566 Zhukovsk,iy, V,.S. Stress and Strain Distribution.in Flat Notched Ba___ rs fn O~ne Bars n onnection With the Three-dimensional Character of the, State of Stress 54 The author investigates stress distribution and concentra- tion in flat steel specimens of varying thiaknesses with deep notches. The relationship between strelss concentration and the thickness of the specimens is shown in diagrams. Lomakin, V.A. Theoretical Determination:of Residual Stresses During Heat Treatment of Metals 72 In this investigation residual stresses accompazlying heat treatment are determined by evaluating plastic deformations occurring during the process and establishing a strass-strain relationship by means of the theory of alasb0plasfto strains.- ,Test calculations of residual stress diatributioit In a quenched cylinder fully agreed with other experimental data. Vagapov# R.D., and 0.1. Shishorina. LateralCompresiqlon of a. Wide Strip With a Hole Near the Edge 84 The work described in this article was done at the Lab- Card 3/4 Problems of Strength (Cont.) SO.V/2366 oratory for Dynamic Strength of Machine Parts Institute of Mechanical Engineering, Academy of Soiencest &'3S;RQ B. I. Rus1kin participated In the experiment. Determination of.the, lateral compression was obtained by a method of superposition involving the solutions for omAidirectional compression and lo4gitudinal tension. An experimental check fully agreed.with the results of the theoretical solution. AVAILABLE: Library of Congress GO/eO Card 4/4 12.;10-59 3/572/60/000/006/009/018 D224/1)304 AUTHORs Zhukovskiy, Ve $0, Candidate,of:Technical Sciencesi ---------------------- TITLE; The stressed state and strength of ai'flat steel bar e a of considerable thicknessin the presenc,' of conc,ehtr.' tion of stresses SOURCE: Raschety na prochnost'j- teoreticheskiye:i eksperimen-' tallnyye issledovaniya-p Irochnosti.mash-inostroitellnykh konstruktsiy. Sbornik atatey. No, 6* Moscow, 196o., 145-154 TEXT: After static fracture of a flat steel bar having dee~~and ,sharp cuts on both sides, two.different zones,:.are obeervedoil the surfaceg one of which (central) indicates failure of:material in the elastic domain (brittle failure), It*ie of intbrest to'com- pare the dimensions of the zones with the results of approximat 'e calculation of stress distribution in the weakene&oross-seation, The author gives a graph of stress distributions calculated from experimental values of deformationsg.with reference' -to previous Card 1/2 nil f3 ........ . 3/572I60/000/006/009/01'8 The stressed state ... D224YD304 publications by himself and others, There are 6~Xigures and 17 re:- ferences: 16 Soviet-bloc and 1 non-Soviet-bloo.;The-reference~to the English-language publication reads as follows: M,.' L. Pried and G Sachs, Notched bar.tension tests on annealed carbon steel sipe- cimens of various sizes and contours. Symposium on deformation ofi metals as related to forming and service. ASTM,'Speoial Technical Publication N87, 1949. Card 2/2 ACC NR1 AT602 /6317/0323 1846 (IV SOURCE CODE: UR/0000/65;/000/000 AUTHOR: ~hjkovskiyft V 3 Madiyevskiy, Ve L; Reznikovicbs K. 1. 34 7 ORG: Hiaher Naval Engineering School im. F4 E. Dz6rzhinskiy(Vysshe-Ye voyenno-morsko,ye inzhenernoye uchilishche) TITLE: The true wall temperature In a stream of superanturated SOURCOE: Teplo- I ina'sooperenos. t. III: Teplo- I me asoporenos famykb prevrasbcheni-yokb (Heat and mass transferoNs 3:- Heat and mass transfer in phase transformations). MInskp Nauke*1 tekhnikap 19650 317-323 TOPIC TAGS: steam power plant, temperature measurement. ABSTRACT: The experimental "nit employed was.fe&fron-sn industrial' boiler which produced slightly moist steam at a pressure.of 16 to 20 atmospheres, After throttling$ this steem4 wbicb was somewhat .~ superheated, was led through a spray type umidifier into a horizontal tank to which was attached the experimental round*noz-,,.10, wbich;bad along its length seven outlets for sampling the pressure at tbelwall:9 The experimental results are presented in the form.of a figure which shows the distribution of the relative tempersturep? p/jO. Further Card 1/2 11 ACC NR. AT6021846 9::p A) AP6021217 R'C'E CODE: UR/0294/661004/003/0399/0406 AUTHOR: Zhukovskiy.- V. S. (Leningrad); Mad~yevskiy,__X, L.' (Leningrad); Reznikovich.~ K. 1. (L ingrad) ORG: none TITLE: On the characteristic temperature of a wall in a stream of supersaturate~d*steam SOURCE: Teplofizika vysokikh temperatur, v. 4, no. 3, 1966, 399-406 TOPIC TAGS: steam superheater,'Laval nozzlep supersonic flow,liquid flow ABSTRACT: The flow of a saturated steam in a Laval nozzle is investigated.by deter- mining the characteristic wall temperature and e femper4ture stagnation coefficient. The review of literature covering such flows indicates incomplete underst a-h.ding of the problem which has been attacked by authors by developing a splacial apparatus allowing stagnation and wall temperature measurements to be made at anY point in the flow. This~. system is described with special attantion paid to the sup~ersonic Ix--gime of tho flow. The measurements have been tabulated for two-to-one relative pr4issure range and sev~- ral superheating conditions. The results satisfy a simple relation for the tempera,- ture dependence of the stagnation coefficient. The characteristic wall temperature corresponds to the results of D. J. Riley in Engineer, 210, 1960. The divergence of results from the theoretical predictions is due to flow conditions where the steam is UDC: 536.423.4:532.5 Card 1/2 -L-4501--66- ACC NRt AP6021217 near the phase-transition state and such initial parameter'-a aa the degree of satura- tions are critical. This has been confirmed by observing.the behavior offlow with artificially introduced liquid phase. It was established 1hal: 'the surface effects which determine the stagnation coefficient are also strongly dependent on the proximi- ty of equilibrium transition point and influence the flow chavacteristics. Orig. art, has: 4 figures, 1 table. SUB COM, 20/ SUBM DATE 05Jan651 ORIG REF: 007/ OTH IM F tQ03 AP 92 66/cOO/006/0018/0021 ACC NRI SOURCE CODE: UR/012ii' AUTHOR; Zhukovskiy, V. S. (Candidate of technical sciences'LLecturer); Surkov,~A. 1. (Candidate of tec 6ai_8'6iences); Morozov, B. A. (Doctor of technical sciehces) -7 ORG: None ''TITLE: Using the net-point method for dqtermining stresses in Lpal. td Vith complex shapes SOURCE: Vestnik mast-linostroyeniyall no. 6, 1966, 18-21 TOPIC TAGS: stress analysis stress concentration stress distribution ABSTRACT: Expressions are given for calculating stresses in,pIrta of.various cbnfig- urations. The net-point method is used for calculating stresses -"n,flat parts.~ A6 example is given for using this method to calculate stresses:ih a blooming millframe. The frame was ass,,uned to be loaded.only- vertically, horizontal, forc6s ~being disregwrde as insignificant. The stress curves obtained by the net point:melhod are comp Iar.ed withi results for a flat frame model studied by the photoelastic method. :The:two metho show satisfactory.agreement. Although the net-point method is-normlilly used for cal- culations where the parts are uniform in thickness, it may be lused for approximate stress determination in parts of nonuniform thickness as well Orig. sit. has: figures, 1 table, 8Lformulas. 13 SUB CODE: 20/ SUBM DATE: none ORIG REP: 007/ OTH IM: 001 L _jr- ;j; 'Card llb