
- •1. Основные понятия и положения 11
- •2. Центральное растяжение и сжатие стержня 17
- •3. Геометрические характеристики плоских сечений 42
- •4. Кручение 49
- •5. Изгиб стержней 57
- •Introduction 173
- •1. Basic concepts and principles 175
- •2. Tension and compression of a bar 181
- •3. Geometric characteristics of cross sections 202
- •4. Torsion 208
- •5. Bending of bars 216
- •Index 405 введение
- •1. Основные понятия и положения
- •1.1. Задачи сопротивления материалов, основные гипотезы и допущения
- •1.2. Типы нагрузок и деформаций
- •1.3. Определение внутренних усилий методом сечений. Напряжения
- •2. Центральное растяжение и сжатие стержня
- •2.1. Напряжения и продольная деформация при растяжении и сжатии
- •2.2. Закон Гука при растяжении и сжатии
- •2.3. Поперечная деформация при растяжении и сжатии
- •2.4. Диаграмма растяжения низкоуглеродистой стали
- •2.5. Потенциальная энергия деформации при растяжении
- •2.6. Расчеты на прочность при растяжении и сжатии
- •2.7. Статически неопределимые задачи
- •2.8. Напряжения в наклонных сечениях при растяжении (сжатии) в одном направлении
- •2.9. Закон парности касательных напряжений
- •2.10. Определение напряжений в наклонных сечениях при растяжении (сжатии) в двух направлениях
- •2.11. Определение главных напряжений и положения главных площадок
- •2.12. Зависимость между деформациями и напряжениями при плоском и объемном напряженных состояниях (обобщенный закон Гука)
- •2.13. Работа внешних и внутренних сил при растяжении (сжатии). Потенциальная энергия деформации
- •3. Геометрические характеристики плоских сечений
- •3.1. Статический момент площади
- •3.2. Полярный момент инерции
- •3.3. Осевой момент инерции
- •3.4. Момент инерции при параллельном переносе осей
- •3.5. Главные оси и главные моменты инерции
- •4. Кручение
- •4.1. Определение крутящего момента
- •4.2. Определение напряжений в стержнях круглого сечения
- •4.3. Деформации и перемещения при кручении валов
- •4.4. Потенциальная энергия при кручении
- •5. Изгиб стержней
- •5.1. Типы опор балок
- •5.2. Определение опорных реакций
- •5.3. Определение внутренних усилий при изгибе
- •5.4. Правило знаков для изгибающих моментов и поперечных сил
- •5.5. Дифференциальные зависимости при изгибе
- •5.6. Построение эпюр изгибающих моментов и поперечных сил
- •5.7. Определение нормальных напряжений
- •5.8. Условия прочности по нормальным напряжениям
- •5.9. Потенциальная энергия деформации при изгибе
- •5.10. Теорема о взаимности работ. Теорема о взаимности перемещений
- •5.11. Определение перемещений методом Мора
- •6. Теории прочности
- •6.1. Назначение гипотез прочности
- •6.2. Первая гипотеза прочности
- •6.3. Вторая и третья гипотезы прочности
- •6.4. Энергетические гипотезы прочности
- •7. Сложное сопротивление
- •7.1. Изгиб в двух плоскостях (косой изгиб)
- •7.2. Изгиб с растяжением (сжатием)
- •7.3. Внецентренное сжатие (растяжение)
- •7.4. Кручение с изгибом
- •7.5. Кручение с растяжением (сжатием)
- •7.6. Пример расчета вала на изгиб с кручением
- •8. Расчет тонкостенных сосудов
- •9. Расчет сжатых стержней на устойчивость (продольный изгиб)
- •9.1. Устойчивые и неустойчивые формы равновесия
- •9.2. Формула Эйлера для критической силы
- •9.3. Влияние способа закрепления концов стержня на критическую силу
- •9.4. Пределы применимости формулы Эйлера
- •9.5. Эмпирические формулы для определения критических напряжений
- •9.6. Практическая формула для расчета на устойчивость
- •10. Динамическое действие нагрузок
- •10.1. Динамические нагрузки
- •10.2. Вычисление напряжений при равноускоренном движении
- •10.3. Определение перемещений и напряжений при ударе
- •11. Расчет на прочность при напряжениях, циклически изменяющихся во времени (расчет на усталость)
- •11.1. Основные определения
- •11.2. Кривая усталости при симметричном цикле. Предел выносливости
- •11.3. Диаграммы предельных напряжений и амплитуд цикла
- •11.4. Факторы, влияющие на предел выносливости
- •11.5. Определение коэффициента запаса прочности при симметричном цикле
- •11.6. Определение коэффициента запаса прочности при асимметричном цикле напряжений
- •Предположим, что при увеличении нагрузки на деталь отношение Такое нагружение называется простым.
- •11.7. Практические меры повышения сопротивления усталости
- •Практикум Лабораторная работа № 1
- •Введение
- •Установка
- •Порядок выполнения
- •Контрольные вопросы
- •Литература
- •Лабораторная работа № 2
- •Введение
- •Установка
- •Порядок выполнения
- •Контрольные вопросы
- •Литература
- •Лабораторная работа № 3
- •Введение
- •Установка
- •Порядок выполнения
- •Introduction
- •Basic concepts and principles
- •Tasks, main hypothesis and assumptions of the strength of materials
- •1.2. Types of loads and deformations
- •1.3. Determining the internal forces by the method of sections. Stresses
- •2. Tension and compression of a bar
- •2.1. Stresses and a longitudinal deformation in tension and compression
- •2.2. Hooke,s law in tension and compression
- •2.3. The transverse deformation in tension and compression
- •2.4. The tension diagram of the lowcarbon steel
- •2.5. The potential deformation energy in tension
- •2.6. Strength calculation in tension and compression
- •2.7. Statically indeterminate problems
- •2.8. Stresses at inclined sections under tension (compression) in one direction
- •2.9. Law of the shearing stresses couple
- •2.10. Determination of stresses at the inclined sections in tension (compression) in two directions
- •2.11. Determining the principal stresses and the principal planes position
- •2.12. The relation between the deformations and the stresses for the plane and general stresses (a general form of Hook’s law)
- •2.13. The work of the external and internal forces in tension (compression). Strain energy
- •3. Geometric characteristics of cross sections
- •3.1. First moment of an area
- •3.2. Polar moment of inertia
- •3.3. Axial moment of inertia
- •3.4. The moment of inertia at parallel displacement of axis
- •3.5. Principal axes and principal moment of inertia
- •4. Torsion
- •4.1. Determining the twisting moment
- •4.2. Determining the stresses in the round section bar
- •4.3. The deformations and displacements in the shaft torsion
- •4.4. Internal strain energy in torsion
- •5. Bending of bars
- •5.1. Types of the beam support
- •5.2. Determining the support reactions
- •5.3. Determining the internal stresses in bending
- •5.4. The sign rule for the bending moments and the shearing forces
- •5.5. The differential relationships in bending
- •I.E. The intensity of the distributed load is equal to the derivative of the shearing force with respect to the bar section abscissa.
- •I.E. The shearing force is equal to the derivative of the bending moment with respect to the bar section abscissa.
- •I.E. The second derivative of the bending moment with respect to the bar section abscissa is equal to the intensity of the distributed load.
- •5.6. Drawing bending moment and shearing force diagrams
- •5.7. Determining the normal stress
- •5.8. Strength conditions with normal stresses
- •5.9. Strain energy in bending
- •5.10. Betty’s reciprocal theorem. Reciprocal displacement theorem
- •5.11. Determining displacements by Mohr’s method
- •6. Strengtn theory
- •6.1. The purpose of strength hypotheses
- •6.2. The first strength hypothesis
- •6.3. The second and third strength hypotheses
- •6.4. The energy hypotheses of strength
- •7. Combined stress
- •7.1. Bending in two planes (non-uniplanar bending)
- •7.2. Combined axial tension (compression) and bending
- •7.3. Eceentrical tension (compression)
- •7.4. Combined torsion and bending
- •7.5. Combined torsion and compression
- •7.6. Example of the shaft calculation in bending with torsion
- •8. Calculation of the thin-walled vessels
- •9. Stability analysis of the bars in compression (buckling)
- •9.1. Stable and unstable equilibrium forms
- •9.2. Euler’s formula for the critical force
- •9.3. Influence of bar end conditions on the critical force
- •9.4. Applicability limits of of Euler’s formula
- •9.5. Empirical formula for determining the critical stresses
- •9.6. The practical formula for the stability analysis
- •10. Dynamic load action
- •10.1. Dynamic load
- •10.2. Calculating stresses under the uniformly accelerated motion
- •10.3. Determining displacements and stresses under the impact
- •11. Stress analysis under the stresses changing cyclically in time
- •11.1. Basic definitions
- •11.2. Fatigue (Wohler’s) curve under the symmetrical cycle. Fatigue strength
- •11.3. The limit stress diagram and the cycle amplitude
- •11.4. Factors influencing on the fatigue strength
- •11.5. Determining the factor of safety under the symmetrical cycle
- •11.6. Determining the factor of safety under the asymmetrical stress cycle
- •11.7. Practical measures to increase the fatigue strength
- •Practicum Laboratory work № 1
- •Introduction
- •Installation
- •Test specimens
- •Test questions
- •Literature
- •Laboratory work № 2
- •Introduction
- •Installation
- •Test questions
- •Literature
- •Laboratory work № 3
- •Introduction
- •Installation
- •Individual task report
- •Test questions
- •Literature
- •Англо-русский терминологический словарь
- •Список фамилий ученых
- •Greek alphabet
- •Сокращения
- •Единицы измерения
- •Список наиболее употребительных знаков
- •Список использованной литературы
- •Алфавитный указатель
- •Сопротивление материалов
- •625000, Тюмень, ул. Володарского, 38.
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Basic concepts and principles
Tasks, main hypothesis and assumptions of the strength of materials
Practice shows that all construction parts are deformed by the load actions i.e. they change their shape and dimensions and in some cases the construction rupture takes place.
The science of the strength and deformation of the machines and construction materials elements is the strength of materials.
The capability of the construction materials and their elements to resist the external forces without breaking is called the strength.
The calculation methods for the strength, stiffness and buckling of construction elements are considered by the strength of materials science.
The strength calculations make it possible to determine the dimensions and shapes of the elements bearing the load under the minimum material expenditure.
Stiffness is the capability of a body or a construction to resist the deformation arising.
The shape and constructions dimentions changes being within the admitted limits are guaranteed by the stiffness calculation.
The stability is the capability of a construction to resist the actions intendiny to move it into a new equilibrium position.
The appearance of large deformations causing a sudden system transition into a new equilibrium shape or a rupture is prevented by stability calculations.
A sudden curvature of a long rectilineal bar compressed along the axis can be an example of buckling.
In practice we deal in most cases with constructions of a complicated shape but they can be presented as consisting of separate simple elements, such as bars, plates, shells.
The basic calculation element in the strength of materials is the bar i.e. a body whose transverse sizes are much lesser compared to its length. The bars can have a straight or curved axis, be of a constant or variable section.
The plane section perpendicular to the bar axis is called the cross section while that parallel to the bar axis is called longitudinal.
Besides the bar calculation the strength of materials considers the calculation of plates and shells i.e. the bodies having smaller thickness compared to other sizes (for example, reservoirs, pipes, ship and plane sheaths). The bodies whose three basic sizes are of commensurable quantities are called massive bodies (e.g. foundations, lathe beds).
The elastic force arising in the body due to its deformation under external force actions resists a deformation and tends to return the body particles to the initial position. The internal force molecule interactions cause the elastic forces.
The strength of materials studies body deformations and internal forces arising under these deformations.
The deformation caused by external force actions can completely or partially disappear when the forces are removed. The capability of materials to eliminate the deformation after the external force actions removal is called elasticity. The deformation disappearing after the external force action removal is called elastic; the deformation not disappearing after the external force action is called residual or plastic. Plasticity is the capability of the material to have a considerable deformation without breaking and the materials are called plastical. Low - carbon steel, aluminum, copper, brass and others are referred to the materials in question.
It should be noted that the rise of considerable residual deformations in many cases brings to the disturbance of the construction normal work and therefore it is inadmissible.
The materials having very small elastity are called brittle. The brittle materials unlike plastical break under the visible residual deformation. Cast iron, hard facing alloys, glass, brick and some others are examples of brittle materials.
The science of the strength of materials is based on the theoretical mechanics laws. The principle of solidification in the strength of materials considered by the theoretical mechanics in the strength of materials will be applied to compose the static equations of equilibrium of the deformed bodies so as to determine the connection reactions and the internal forces in details sections.
Hypotheses and assumptions in the subject of the strength of materials. All real bodies have the complicated pattern construction, hollownesses, heterogeneous inclusions which have the dimensions much lesser than the dimensions of the bodies. The mentioned peculiarities of the materials are impossible to take into account because of their chaotic nature and volume distribution, therefore a number of the hypotheses and assumptions are accepted. These are:
The material is to be as follows
solid (we ignore the atom structure, hollownesses and inclusions);
homogeneous (a material has the same properties in all volume points);
isotropic (a material has the same properties in all directions).
The body does not have any internal forces before the external forces are applied.
All materials are ideal elastic ones (bodies take their initial shape and dimensions when the external load is entirely removed).
The change values of the dimensions and shape depend on the external load linear and are small compared to the body dimensions.
The plane body section before and after the deformation remains the same.
The mentioned conditions allow one to receive the principle of the superposition i.e. the result of the system forces action is equal to the sum of the action results of each force of this system when the force is applied in turns and in any order possible.