scholarly journals Dependence of the stress-strain state of the ice cover on its physical and mechacal properties under conditions of bending-gravitational resonance

Author(s):  
В.М. Козин

Рассмотрено влияние физико – механических характеристик льда на напряженно-деформированное состояние (НДС) ледяного покрова при его деформировании изгибно – гравитационными волнами (ИГВ), возбуждаемыми движущейся по льду нагрузкой с резонансной скоростью, т.е. в условиях изгибно-гравитационного резонанса (ИГР). Исследования проведены с целью дальнейшего изучения возможностей резонансного метода разрушения ледяного покрова (РМРЛ), осуществляемого судами на воздушной подушке (СВП). Отмечено, что в определенных ледовых условиях РМРЛ может оказаться эффективнее существующих традиционных технологий разрушения ледяного покрова. Перечислены основные физико-механические свойства льда, влияющие на НДС ледяного покрова в условиях ИГР. Приведены наиболее вероятные диапазоны их изменения. Задача о деформировании ледяного покрова перемещающейся по нему распределенной нагрузкой рассматривается в линейной постановке. Лёд моделируется изотропной пластиной бесконечной протяжённости, поведение которой описывается реологической вязко – упругой моделью Кельвина – Фойгта. Работоспособность полученных зависимостей проверена путем сопоставления результатов численных расчётов прогибов льда с данными натурных экспериментов. Приведены результаты теоретических исследований влияния на НДС ледяного покрова изменения параметров основных физико-механических характеристик льда в пределах их наиболее вероятного диапозона изменения при резонансной скорости движения нагрузки. Сделан вывод, что при расчетах НДС ледяного покрова в условиях ИГР, т.е. при определении толщины ледяного покрова, разрушаемого СВП резонансным методом, следует уточнять только значение модуля Юнга для конкретных ледовых условий. Остальные характеристики льда можно выбирать в соответствии с их осредненными значениями. The influence of the physical and mechanical characteristics of ice on the stress – strain state (SSS) of the ice cover when it is deformed by bending-gravitational waves (IGW) caused by a load moving along the ice at a resonant speed, i.e. under conditions of bending – gravitational resonance (IGR), is considered. The research was conducted in order to further study the possibilities of the resonant method of ice cover destruction (RMRL), carried out by hovercraft (SVP). It is noted that in certain ice conditions, RMRL can be more effective than existing traditional technologies of ice cover destruction. The main physical and mechanical properties of ice that affect the VAT of the ice cover in the conditions of GAMES are listed. The most probable ranges of their changes are given. The problem of ice cover deformation by a distributed load moving along it is considered in a linear formulation. Ice is modeled by an isotropic plate of infinite extent, the behavior of which is described by the rheological viscoelastic Kelvin-Voigt model. The efficiency of the obtained dependences was verified by comparing the results of numerical calculations of ice deflections with the data of field experiments. The results of theoretical studies of the influence of changes in the values of the main physical and mechanical characteristics of ice within their most probable range of changes at the resonant speed of the load movement on the ice cover VAT are presented. It is concluded that when calculating the VAT of ice cover in the conditions of GAMES, i.e. when determining the thickness of the ice cover destroyed by the SVP resonance method, it is necessary to specify only the value of the Young's modulus for specific ice conditions. Other ice characteristics can be selected according to their averaged data.

2015 ◽  
Vol 56 (5) ◽  
pp. 920-926 ◽  
Author(s):  
A. V. Pogorelova ◽  
V. M. Kozin ◽  
A. A. Matyushina

2019 ◽  
Vol 97 ◽  
pp. 04009 ◽  
Author(s):  
Karim Sultanov ◽  
Pavel Loginov ◽  
Sabida Ismoilova ◽  
Zulfiya Salikhova

Mechanical characteristics of soils under dynamic and static loads are determined in laboratory conditions on special devices. Dynamic loads in the devices are initiated by an impact on a soil sample. Under the impact the waves are initiated in soil; they significantly affect the stress-strain state of soil samples placed in the device. Depending on the parameters of the impact load in the device, in different sections of soil sample there arise the stress-strain states, different in quality and quantity. Mechanical characteristics of soil, determined by this stress-strain state, also differ. The effect of stress-strain state of soil on its mechanical characteristics can be estimated theoretically. The initiation of the wave process and dynamic stress-strain state in soil sample placed in the device can be theoretically examined in detail. In this regard, the wave problem is set, which corresponds to the statement of experiments on the device of dynamic loading of soil. The law of soil strain is taken as an elastic-viscoplastic one. Numerical solution of wave equations is obtained by the finite difference method. Based on the analysis of stress-strain state of soil in various sections, obtained by numerical calculations, the condition is derived under which the effect of wave processes on mechanical characteristics of soils is eliminated. This condition (formula) establishes the relationship between the wavelength, the velocity of wave propagation in soil, the thickness of the soil sample in the device and the duration of dynamic load.


Author(s):  
А. Г. Гребеников ◽  
И. В. Малков ◽  
В. А. Урбанович ◽  
Н. И. Москаленко ◽  
Д. С. Колодийчик

The analysis of the design and technological features of the tail boom (ТB) of a helicopter made of polymer composite materials (PCM) is carried out.Three structural and technological concepts are distinguished - semi-monocoque (reinforced metal structure), monocoque (three-layer structure) and mesh-type structure. The high weight and economic efficiency of mesh structures is shown, which allows them to be used in aerospace engineering. The physicomechanical characteristics of the network structures are estimated and their uniqueness is shown. The use of mesh structures can reduce the weight of the product by a factor of two or more.The stress-strain state (SSS) of the proposed tail boom design is determined. The analysis of methods for calculating the characteristics of the total SSS of conical mesh shells is carried out. The design of the tail boom is presented, the design diagram of the tail boom of the transport category rotorcraft is developed. A finite element model was created using the Siemens NX 7.5 system. The calculation of the stress-strain state (SSS) of the HC of the helicopter was carried out on the basis of the developed structural scheme using the Advanced Simulation module of the Siemens NX 7.5 system. The main zones of probable fatigue failure of tail booms are determined. Finite Element Analysis (FEA) provides a theoretical basis for design decisions.Shown is the effect of the type of technological process selected for the production of the tail boom on the strength of the HB structure. The stability of the characteristics of the PCM tail boom largely depends on the extent to which its design is suitable for the use of mechanized and automated production processes.A method for the manufacture of a helicopter tail boom from PCM by the automated winding method is proposed. A variant of computer modeling of the tail boom of a mesh structure made of PCM is shown.The automated winding technology can be recommended for implementation in the design of the composite tail boom of the Mi-2 and Mi-8 helicopters.


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