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Datum:2012
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Sprache:English
Veröffentlicht: Інститут проблем міцності ім. Г.С. Писаренко НАН України 2012
Schriftenreihe:Проблемы прочности
Online Zugang:http://dspace.nbuv.gov.ua/handle/123456789/173117
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Zitieren:Abstracts // Проблемы прочности. — 2012. — № 6. — С. 168-170. — англ.

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spelling irk-123456789-1731172020-11-22T01:26:38Z Abstracts 2012 Article Abstracts // Проблемы прочности. — 2012. — № 6. — С. 168-170. — англ. 0556-171X http://dspace.nbuv.gov.ua/handle/123456789/173117 en Проблемы прочности Інститут проблем міцності ім. Г.С. Писаренко НАН України
institution Digital Library of Periodicals of National Academy of Sciences of Ukraine
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language English
format Article
title Abstracts
spellingShingle Abstracts
Проблемы прочности
title_short Abstracts
title_full Abstracts
title_fullStr Abstracts
title_full_unstemmed Abstracts
title_sort abstracts
publisher Інститут проблем міцності ім. Г.С. Писаренко НАН України
publishDate 2012
url http://dspace.nbuv.gov.ua/handle/123456789/173117
citation_txt Abstracts // Проблемы прочности. — 2012. — № 6. — С. 168-170. — англ.
series Проблемы прочности
first_indexed 2025-07-15T09:39:15Z
last_indexed 2025-07-15T09:39:15Z
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fulltext Lebedev A. A., Golubovskii E. R., Lokoshchenko A. M., Muzyka N. R., Lamashevskii V. P., Shvets V. P., and Efimenko E. V. Assessment of the Limiting Levels of Dispersed Damage in Materials under Steady-State Conditions of Static and Cyclic Loading // Problems of Strength. – 2012. – No. 6. – P. 5–13. The results on the analysis of possible ways of using the concept of dispersed defects in prac- tice when making the admissible damage analy- sis of structures are presented. The experimental data on the limiting damage to some alloys widely used in mechanical engineering, which are obtained by the LM-hardness method using specimens fractured after the operating time un- der conditions of creep and cyclic fatigue, are processed and generalized. A linear correlation is found between the levels of the limiting dam- age and working stresses during the operating time. A version of the procedure for determining the parameters of the correlating equation from the results of basic experiments is proposed. Gulenko A. G., Buchatskii A. A., Margolin B. Z., Kashtanov A. D., and Fedorova V. A. A Study of Crack Propagation in Austenitic Steels under Creep Conditions Including the Influence of Thermal Pre-Ageing // Problems of Strength. – 2012. – No. 6. – P. 14–33. Based on processing of a large body of experi- mental data obtained for austenitic steels 304 and 316, the authors have determined the coeffi- cients for the equation of crack growth rate as a function of the C*-integral under creep condi- tions. To analyze applicability of this equation to Russian austenitic steels, an investigation of the crack growth rate was carried out for the base metal, weld, and heat-affected zone in steels 10Kh18N9 and 08Kh16N11M3 in the ini- tial (austenized) state and upon a long-term ther- mal ageing. The authors propose a method of how to allow for thermal ageing in the calcula- tions of the crack growth rate under creep condi- tions. Orynyak I. V., Yakovleva E. S., and Dubik Ya. R. The Application of the Combined Method of Weight Functions for the Determination of a Through-Wall Crack Opening Area in a Shell // Problems of Strength. – 2012. – No. 6. – P. 34– 55. The crack opening area of a through-wall crack in a shell is one of the main design parameters in the leak-before-break concept. The available methods for determining this parameter essen- tially consider the shell as a plane body and disre- gard the linearly varying component of the displacement field (as in the plate theory). Based on a combined method of weight functions, a simple procedure is put forward to derive an ap- proximate expression for the fundamental field of displacements under the action of a concen- trated force and moment onto the crack faces in the form of a sum of a uniform component and a component that linearly varies through the wall thickness. This provides, in particular, conve- nient formulas to find the crack opening area in a polynomial field of membrane stresses as well as linear ones. For a cylindrical shell with a lon- gitudinal or transverse crack, the calculated val- ues of the crack opening area are compared with those reported elsewhere. The contribution of the linear component to the total crack opening area is assessed. Kharchenko V. K. and Bukhanovskii V. V. High-Temperature Strength of Refractory Metals, Alloys and Composite Materials Based on Them. Part 2. Molybdenum and Niobium Alloys // Problems of Strength. – 2012. – No. 6. – P. 56–66. The results of investigations of the mechanical characteristics of molybdenum and niobium al- loys and their welded joints, which are used in space-rocket hardware, have been generalized. The investigations were carried out under short- time, sustained static and low-cycle loading con- ditions on small time bases in a temperature range of 290–2270 K. Matokhnyuk L. E., Yakovleva T. Yu. , and Byalonovich A. V. Prediction of Gigacycle Fatigue Resistance Characteristics of Metals from High-Frequency Test Data. Part 2. Application of Fatigue Damage Accumulation Model // Problems of Strength. – 2012. – No. 6. – P. 67–80. A model of formation and development of local plastic strain regions is proposed on the basis of an analysis of the main physical processes tak- ing place in a metallic material under the action of cyclic loads. An equation of material state for the instant of time directly preceding fatigue Abstracts 168 ISSN 0556-171X. Ïðîáëåìû ïðî÷íîñòè, 2012, ¹ 6 crack initiation has been derived, in which cy- clic loading frequency in explicit form as a fac- tor directly affecting the damage accumulation rate and stress ratio are taken into account. The equation is the basis for the prediction of fatigue resistance characteristics, large loading bases as well, at different frequencies, including low ones, from high-frequency test data. Stepanov G. V., Babutskii A. I., Chizhik A. V., and Gromov V. E. Pulse Electric Current Effect on Mechanical Properties of Titanium Aluminide Produced by the Self-Propagating High-Temperature Synthesis Technique // Problems of Strength. – 2012. – No. 6. – P. 81– 92. We present results of study on the effect of pulse electric current treatment on bending strength and hardness of intermetallic titanium aluminide produced by the self-propagating high-temperature synthesis technique. It is shown such treatment results in some increase in strength and plasticity of the intermetallide in comparison with the initial state, while its hard- ness decreases. The results of microstructural analysis show that reduction of the material brit- tleness after treatment is a consequence of cur- rent-induced change of thin structure of a material, redistribution of pores and reduction of the residual tensile stresses. Chirkov A. Yu. Construction of Two-Level Integration Schemes for the Equations of Plasticity in the Theory of Deformation along the Paths of Small Curvature // Problems of Strength. – 2012. – No. 6. – P. 93–124. The construction of a set of two-level integra- tion �-schemes for the equations of the flow the- ory of plasticity, describing anisothermic loading processes along the deformation paths of small curvature, is described. In this case, a stress- strain state is dependent on thermomechanical loading history, and inelastic deformation should be followed over the whole examined time interval in step solving the boundary prob- lem. Basic concepts of the phenomenological model are built upon the Prandtl–Reuss equa- tions of plasticity and the Huber–Mises yield condition. The loading process is divided into several time steps. The equations of plasticity are integrated in a loading step. The general pro- cedure of transformations to construct a set of two-level integration �-schemes for the equa- tions of plasticity is proposed. The conditions for the agreement between the considered equa- tions of plasticity and the principle of work irre- versibility with plastic strain increments and Drucker’s hardening postulate are formulated. As an example, illustrating the properties of these equations, the deformation problem is solved for a thin-walled round pipe subject to ax- ial tension and torsional moment. Results of solv- ing the model problem, obtained with different two-level integration schemes, are presented. Practical recommendations as to the choice of the parameter � are given. Karachun V. V. and Mel’nik V. N. Elastic Stress State of a Floating-Type Suspension in the Acoustic Field. Deviation of the Spin Axis // Problems of Strength. – 2012. – No. 6. – P. 125– 136. The nature of the elastic interaction between the floating-type suspension of a differentiating gy- roscope and the penetrating acoustic radiation is analyzed, and the computational models of this phenomenon are constructed. The mechanism of occurrence of additional errors in the gyroscopic angular velocity sensor induced by the diffrac- tion phenomena in the moving part of the device is disclosed. The vector diagrams explain the es- sence of the spin axis deviation in the reverberated space. Shul’zhenko N. G., Zaitsev B. F., Vikman N. E., and Asaenok A. V. Vibration Analysis of Rotor with a “Breathing” Crack Using Three- Dimensional Model // Problems of Strength. – 2012. – No. 6. – P. 137–145. A procedure for analyzing vibrations in cracked body using three-dimensional model is pre- sented. The process of “breathing” is described by conditions of contact between the crack faces. Some example calculations are provided. Mazahery A. and Shabani M. O. Mechanical Properties of A356 Matrix Composites Reinforced with Nano-SiC Particles // Problems of Strength. – 2012. – No. 6. – P. 146–155. Metal matrix composites form one group of the new engineered materials in which a strong ce- ramic reinforcement is incorporated into a metal matrix to improve its properties including spe- cific strength, specific stiffness, wear resistance, excellent corrosion resistance and high elastic modulus. A compocasting method was em- ployed to incorporate SiC nano-particles into the aluminum alloy and fabricate metal matrix nanocomposites with uniform reinforcement dis- tribution. Microstructural characterization of compocast composites show a uniform distribu- Abstracts ISSN 0556-171X. Ïðîáëåìû ïðî÷íîñòè, 2012, ¹ 6 169 tion of nano-particles, grain refinement of alumi- num matrix, and presence of the minimal porosity. It was revealed that the presence of nano-SiC reinforcement led to significant im- provement in hardness, 0.2% yield strength and UTS while the ductility of the aluminum matrix is retained. Sedighi M. and Honarpisheh M. Investigation of Cold Rolling Influence on Near Surface Residual Stress Distribution in Explosive Welded Multilayer // Problems of Strength. – 2012. – No. 6. – P. 156–162. The aim of this study is to investigate the effect of cold rolling on residual stress distribution of aluminum and copper three-ply clad sheets fabri- cated by explosive welding. After preparation of the explosive-welded multilayer, explosive- welded Al/Cu/Al specimens were rolled at 11, 30, 40, and 56% thickness reduction. The through-depth residual stress profiles near the surface have been extracted for explosive- welded and cold-rolled multilayers by incremen- tal hole-drilling method. Results show that the surface of explosive-welded multilayer is sub- jected to high tensile residual stresses and will be reduced by cold rolling process. Also, tensile residual stress at the surface of cold-rolled multilayers increases at higher thickness reduction. Fedorenko B. F. and Luk’yanov V. S. Assessment of Endurance Limit of Shafts via Model Test Results // Problems of Strength. – 2012. – No. 6. – P. 163–167. The procedure for assessment of the endurance limit of the eccentric shaft for horizontal forging machine using the results from tests on its geo- metrically similar models has been proposed. The assessment is performed using the analyti- cal relation derived by the dimensional analysis method. Abstracts Âíèìàíèþ ïîäïèñ÷èêîâ! Ïîäïèñàòüñÿ íà æóðíàë «Ïðîáëåìû ïðî÷íîñòè» ìîæíî, êàê îáû÷íî, â ìåñòíûõ îòäåëåíèÿõ ñâÿçè. Æóðíàë âêëþ÷åí â êàòàëîãè Óêðàèíû è Ðîññèè. Íàø èíäåêñ – 70730. Ïîäïèñêó Âû ìîæåòå îôîðìèòü íåïîñðåäñòâåííî â ðåäàêöèè æóðíàëà ñ ëþáîãî î÷åðåäíîãî íîìåðà. Öåíà îäíîãî íîìåðà ñ ó÷åòîì ïî÷òîâûõ ðàñõîäîâ â 2013 ãîäó ñîñòàâèò: â ïðåäåëàõ Óêðàèíû 30 ãðí.; çà ïðåäåëàìè Óêðàèíû 300 ðîñ. ðóá. (~ 10.0 USD). Ïî÷òîâûå ïåðåâîäû íàïðàâëÿòü ïî àäðåñó: 01014, Êèåâ–14, óë. Òèìèðÿçåâñêàÿ, 2. Ðåäàêöèÿ æóðíàëà «Ïðîáëåìû ïðî÷íîñòè» Øèíêàðåíêî Íèíå Ìèõàéëîâíå. Ñïðàâêè ïî òåëåôîíó: (044) 286 5657. Îòäåëüíûì ïèñüìîì íåîáõîäèìî ñîîáùèòü â ðåäàêöèþ òðåáóåìîå êîëè- ÷åñòâî íîìåðîâ, ñóììó è äàòó îòïðàâêè ïåðåâîäà, óêàçàòü ñâîé ïî÷òîâûé àäðåñ. Îòïðàâêà æóðíàëîâ îñóùåñòâëÿåòñÿ ïîñëå ïîñòóïëåíèÿ äåíåã ïîäïèñ- ÷èêà. 170 ISSN 0556-171X. 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De gemaakte PDF-documenten kunnen worden geopend met Acrobat en Adobe Reader 5.0 en hoger.) /NOR <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> /PTB <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> /SUO <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> /SVE <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> /ENU (Use these settings to create Adobe PDF documents for quality printing on desktop printers and proofers. 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