Search Results for “Fedorov V. M.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 05 Nov 2024 21:13:41 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Fedorov V. M.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures https://journal.yuzhnoye.com/content_2024_1-en/annot_6_1_2024-en/ Mon, 17 Jun 2024 07:56:18 +0000 https://journal.yuzhnoye.com/?page_id=34992
M., Fedorov V.M., Triasuchev L.M. M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V.
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6. New methods of load-carrying capacity prediction for the ultimately compressed frame structures

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine,1; Kharkiv Aviation Institute, Kharkiv, Ukraine2

Page: Kosm. teh. Raket. vooruž. 2024, (1); 51-60

DOI: https://doi.org/10.33136/stma2024.01.051

Language: English

Annotation: Amid acute problems that arise in the field of rocket and space technology, mechanical engineering, and other fields and require a workable engineering solution, the problem of prediction and prevention of the unpredicted collapse of the structural members of the structures subjected to loading is considered. Prediction of the load-carrying capacity and residual life of the space frames during the long-term operation is based on the analysis of the stress and strain state, using readings from the strain and displacement pickups installed in the most loaded zones. In this case the yield strength of the structural material or the fatigue strength of the material may be considered as the criterion of the maximum load. At the same time the loss of stability of the compressed structural members used in the load-carrying thin-walled structures are among the potentially dangerous failure modes. In these cases such failure occurs unexpectedly without any visible signs of change in the initial geometry. Application of the adequate diagnostic techniques and methods of prediction of the maximum loads under compression conditions will make it possible to avoid the structural failures. In this case an assembly under test may be used for other purposes. To perform static strength testing, the rocket and space companies use costly compartments of as-built dimension. Therefore, keeping compartments safe solves an important problem of saving financial costs for hardware production. Nowadays this problem is particularly acute when ground testing the new technology prototypes.

Key words: space frames, load-carrying members, stress and strain state, loss of stability, prediction of the structural failure.

Bibliography:
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  2. Truesdell C. A first course in rational continuum mechanics. The Johns Hopkins University, Baltimore, Maryland, 1972. Russian translation was published by Mir, M., 1975. P. 592.
  3. Rabotnov Yu. Mehanika deformiruyemogo tverdogo tela.: Nauka, 1979. S. 744.
  4. Bolotin V. Nekonservativnyie zadachi teoriyi uprugoy ustoychivosti. Phyzmatgiz, M., 1961. S. 339.
  5. Feodosyev V. Izbrannyie zadachi i voprosy po soprotivleniyu materialov. Nauka. , 1973. S. 400.
  6. Muliar Yu. M., Fedorov V.M., Triasuchev L.M. O vliyanii nachalnyh nesovershenstv na poteryu ustoychivosti sterzhney v usloviyah osevogo szhatiya. Kosmicheskaya tehnicka. Raketnoye vooruzheniye: Sb. nauch.-tehn. st. 2017. Vyp. 1 (113). S. 48-58. https://doi.org/10.15193/zntj/2017/113/210
  7. Volmir A. Ustoychivost deformiruyemyh sistem. M., 1967. S. 984.
  8. Muliar Yu. M. K voprosy ob ustoichivosty szhatogo sterzhnya. Tekhnicheskaya mekhanika. Dnepropetrovsk: ITM. 2000. No S. 51.
  9. Muliar Yu. M., Perlik V.I. O matematicheskom modelnom predstavlenii informatsionnogo polia v nagruzhennoy deformiruyemoy sisteme. Informatsionnyie i telekommunikatsionnyie tehnologii. M.: Mezhdunar. akad. nauk informatizatsii, informatsionnyh protsessov i tehnologiy. 2012. No 15. S. 61.
  10. Koniuhov S. N., Muliar Yu. M., Privarnikov Yu. K. Issledovaniye vliyaniya malyh vozmuschayuschih vozdeystviy na ustoychivost obolochki. Mehanika. 1996. 32,  No 9. S. 50-65.
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6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures
6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures
6.1.2024 New methods of load-carrying capacity prediction for the ultimately compressed frame structures

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23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body https://journal.yuzhnoye.com/content_2018_2-en/annot_23_2_2018-en/ Thu, 07 Sep 2023 12:35:25 +0000 https://journal.yuzhnoye.com/?page_id=30813
M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V.
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23. On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (2); 190-206

DOI: https://doi.org/10.33136/stma2018.02.190

Language: Russian

Annotation: Presented is the theoretical justification of the phenomenon of the inertia initiation under accelerated motion of the body, and gravity origin in the circumterrestrial space. There is no description of the physical nature of the inertia and gravity in the scientific publications. In the phenomenological approach under study, allowing for reflection properties of the space, earlier unknown interdependent information-physical link of the body and its mechanical particles with space under the accelerated motion was determined in the state of rest of the gravitation field as well as in the state of weightlessness. Alongside with the environment, eigenspace, i.e. configuration space of the body and corresponding metric lines of the space are considered. Idea of metric lines agrees with the concept of F. Wilczek, the American physicist, Nobel-Prize laureate, on the existence of the unobservable metric field in the real space. Solution of the problem rests on the example of the cantilever beam and mathematical model of the information reflection process, which for the first time takes into consideration previously unknown property of space reflection. Under the accelerated motion of the body reflection gains the acceleration vector dt d а     . In this case reflection manifests itself in the initiation of the beam of polarization vector under study   ~ in every point of the configuration space and is expressed as     ~ а . Value of the polarization vector equals the value of acceleration vector with negative sign. As a result metric lines of the configuration space under conditions of beam acceleration become polarized lines, generating vector information inertia field. Interaction of mechanical particles with the information inertia field in the configuration space generates physical inertia field of force, providing the real inertia under accelerated motion of the beam. (Relatively slow motion of bodies is studied as compared to the speed of light). According to the set forth unconventional approach the nature of the earth gravity is conditioned by the polarization of the radial metric lines of the circumterrestrial space. And polarization vector is directed to the center of the Earth and equals acceleration vector of the free fall with the same sign. Interaction of the body with specific mass with the vector information field of the Earth generates the physical force field of gravity. Article deals with the fundamental issues of theoretical physics and other fields of natural science. Materials of the conducted research are regarded as a potential scientific discovery.

Key words: configuration space, modified method of sections, information and vacuum environment, metric lines, property of space reflection, polarization, scalar information field, vector information field

Bibliography:
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6. Mulyar Y. M., Perlik V. I. On Mathematical Model Representation of Information Field in Loaded Deformed System. Information and Telecommunication Technologies. М., 2012. No. 15. P. 61-74.
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8. Ursul A. D. Reflection and Information. М., 1973. 231 p.
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11. Cacku M. Physics of Impossible / Translation from English. М., 2016. 456 p.
12. Proceedings of the International Scientific Conference “Problems of Ideality in Science”. М., 2001. 352 p.
13. Mulyar Y. M., Fyodorov V. M., Tryasuchev L. M. On the Impact of Initial Imperfections on Rod Stability Loss in Conditions of Axial Compression. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2017. Issue 1 (113). P. 48-58.
14. Dyomin A.I. Paradigm of Dualism. Space – Time, information – energy. М., 2007. 320 p.
15. Lisin A.I. Paradigm of Dualism. Ide: Reality of ideality. Part 1. М., 1999. 382 p.
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23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body
23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body
23.2.2018 On the Role of Space in Origination of Inertia Force Field, Earth Gravity Force Field and Zero Gravity of Material Body

Keywords cloud

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8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions https://journal.yuzhnoye.com/content_2017_1/annot_8_1_2017-en/ Tue, 27 Jun 2023 12:02:02 +0000 https://journal.yuzhnoye.com/?page_id=29430
M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V. M., Fedorov V.
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8. Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (1); 48-58

Language: Russian

Annotation: The experimental and theoretical justification is presented for the phenomenon of sudden buckling with dynamic effect at stability loss of a rectilinear rod with real existing imperfections. The interdependent connection is established between the initial imperfections and buckling intensity in the effect of zero rigidity of an utmost compressed rod at stability loss in the large.

Key words:

Bibliography:
1. Feodos’yev V. I. Selected Tasks and Problems of Materials Strength. М., 1973. 400 p.
2. Trusdell K. Primary Course of Rational Mechanics of Continuous Media / Translation from English. М., 1975. 522 p.
3. Bolotin V. V. Nonconservative Problems of Elastic Stability Theory. М., 1961. 339 p.
4. Rabotnov Y. N. Mechanics of Deformed Solid Body. М., 1979. 744 p.
5. Konyukhov S. N., Mulyar Y. M., Privarnikov Y. K. Investigation of Minor Disturbing Actions on Shell Stability. Applied Mechanics. 1996. Issue 32, No. 9. P. 59-65.
6. Larionov I. F., Mulyar Y. M., Petushenko Y. G. On Physical Substantiation of Spontaneous Change of Initial Shape of Extremely Compressed Launch Vehicle Bays. Cosmonautics and Rocket Building. Kaliningrad, 2001. Issue 24. P. 129–136.
7. Haken G. Synergetics: Instability Hierarchies in Self-Organizing Systems and Devices / Translation from English. М., 1985. 423 p.
8. Volmir A. S. Stability of Deformed Systems. М., 1967. 984 p.
9. Larionov I. F., Mulyar Y. M., Privarnikov Y. K. Investigation of Local Raising of Shell Structures at Stability Loss of their Bays. Cosmonautics and Rocket Building. Kaliningrad, 1998. Issue 13. P. 92–98.
10. Mulyar Y. M., Perlik V. I. On Prediction of Destruction of Extremely Compressed Launch Vehicle Bays. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2010. Issue 2. P. 28–39.
11. Hoff N. Longitudinal Bending and Stability. М., 1955. 154 p.
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8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions
8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions
8.1.2017 Initial Imperfection Effect on Loss of Rod Stability under Axial Compression Conditions
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