buckling

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1. flamboyantly reckless and boastful behavior

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出典(authority):フリー百科事典『ウィキペディア（Wikipedia）』「2017/05/03 08:05:04」(JST)

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For other uses, see Buckling (disambiguation).

Not to be confused with buckle.

In science, buckling is a mathematical instability that leads to a failure mode.

When a structure is subjected to compressive stress, buckling may occur. Buckling is characterized by a sudden sideways deflection of a structural member. This may occur even though the stresses that develop in the structure are well below those needed to cause failure of the material of which the structure is composed. As an applied load is increased on a member, such as a column, it will ultimately become large enough to cause the member to become unstable and it is said to have buckled. Further loading will cause significant and somewhat unpredictable deformations, possibly leading to complete loss of the member's load-carrying capacity. If the deformations that occur after buckling do not cause the complete collapse of that member, the member will continue to support the load that caused it to buckle. If the buckled member is part of a larger assemblage of components such as a building, any load applied to the buckled part of the structure beyond that which caused the member to buckle will be redistributed within the structure.

In a mathematical sense, buckling is a bifurcation in the solution to the equations of static equilibrium. At a certain point, under an increasing load, any further load is able to be sustained in one of two states of equilibrium: a purely compressed state (with no lateral deviation) or a laterally-deformed state.

Columns

A column under a concentric axial load exhibiting the characteristic deformation of buckling

The eccentricity of the axial force results in a bending moment acting on the beam element.

The ratio of the effective length of a column to the least radius of gyration of its cross section is called the slenderness ratio (sometimes expressed with the Greek letter lambda, λ). This ratio affords a means of classifying columns and their failure mode. The slenderness ratio is important for design considerations. All the following are approximate values used for convenience.

If the load on a column is applied through the center of gravity (centroid) of its cross section, it is called an axial load. A load at any other point in the cross section is known as an eccentric load. A short column under the action of an axial load will fail by direct compression before it buckles, but a long column loaded in the same manner will fail by springing suddenly outward laterally (buckling) in a bending mode. The buckling mode of deflection is considered a failure mode, and it generally occurs before the axial compression stresses (direct compression) can cause failure of the material by yielding or fracture of that compression member. However, intermediate-length columns will fail by a combination of direct compressive stress and bending.

In particular:

• A short steel column is one whose slenderness ratio does not exceed 50; an intermediate length steel column has a slenderness ratio ranging from about 50 to 200, and its behavior is dominated by the strength limit of the material, while a long steel column may be assumed to have a slenderness ratio greater than 200 and its behavior is dominated by the modulus of elasticity of the material.
• A short concrete column is one having a ratio of unsupported length to least dimension of the cross section equal to or less than 10. If the ratio is greater than 10, it is considered a long column (sometimes referred to as a slender column).
• Timber columns may be classified as short columns if the ratio of the length to least dimension of the cross section is equal to or less than 10. The dividing line between intermediate and long timber columns cannot be readily evaluated. One way of defining the lower limit of long timber columns would be to set it as the smallest value of the ratio of length to least cross sectional area that would just exceed a certain constant K of the material. Since K depends on the modulus of elasticity and the allowable compressive stress parallel to the grain, it can be seen that this arbitrary limit would vary with the species of the timber. The value of K is given in most structural handbooks.

The theory of the behavior of columns was investigated in 1757 by mathematician Leonhard Euler. He derived the formula, the Euler formula, that gives the maximum axial load that a long, slender, ideal column can carry without buckling. An ideal column is one that is perfectly straight, made of a homogeneous material, and free from initial stress. When the applied load reaches the Euler load, sometimes called the critical load, the column comes to be in a state of unstable equilibrium. At that load, the introduction of the slightest lateral force will cause the column to fail by suddenly "jumping" to a new configuration, and the column is said to have buckled. This is what happens when a person stands on an empty aluminum can and then taps the sides briefly, causing it to then become instantly crushed (the vertical sides of the can understood as an infinite series of extremely thin columns). The formula derived by Euler for long slender columns is given below.

$F={\frac {\pi ^{2}EI}{(KL)^{2}}}$

To get the mathematical demonstration read: Euler's critical load

where

$F$ = maximum or critical force (vertical load on column),

$E$ = modulus of elasticity,

$I$ = area moment of inertia of the cross section of the column,

$L$ = unsupported length of column,

$K$ = column effective length factor, whose value depends on the conditions of end support of the column, as follows.

For both ends pinned (hinged, free to rotate), $K$ = 1.0.

For both ends fixed, $K$ = 0.50.

For one end fixed and the other end pinned, $K$ ≈ 0.7071.

For one end fixed and the other end free to move laterally, $K$ = 2.0.

$$

 
   
     
       K
       L
     
   
   {\displaystyle KL}
 

is the effective length of the column.

Examination of this formula reveals the following interesting facts with regard to the load-bearing ability of slender columns.

1. The elasticity of the material of the column and not the compressive strength of the material of the column determines the column's bucking load.
2. The buckling load is directly proportional to the second moment of area of the cross section.
3. The boundary conditions have a considerable effect on the critical load of slender columns. The boundary conditions determine the mode of bending of the column and the distance between inflection points on the displacement curve of the deflected column. The inflection points in the deflection shape of the column are the points at which the curvature of the column changes sign and are also the points at which the column's internal bending moments of the column are zero. The closer the inflection points are, the greater the resulting axial load capacity (bucking load) of the column.

A demonstration model illustrating the different "Euler" buckling modes. The model shows how the boundary conditions affect the critical load of a slender column. Notice that the columns are identical, apart from the boundary conditions.

A conclusion from the above is that the buckling load of a column may be increased by changing its material to one with a higher modulus of elasticity (E), or changing the design of the column's cross section so as to increase the its moment of inertia. The latter can be done without increasing the weight of the column by distributing the material as far from the principal axis of the column's cross section as possible. For most purposes, the most effective use of the material of a column is that of a tubular section.

Another insight that may be gleaned from this equation is the effect of length on critical load. Doubling the unsupported length of the column quarters the allowable load. The restraint offered by the end connections of a column also affects its critical load. If the connections are perfectly rigid (does not allowing rotation of its ends), the critical load will be four times that for a similar column where the ends are pinned (allowing rotation of its ends).

Since the radius of gyration is defined as the square root of the ratio of the column's moment of inertia about an axis to its cross sectional area, the above Euler formula may be reformatted by substituting the radius of gyration A·r² for I:

$\sigma ={\frac {F}{A}}={\frac {\pi ^{2}E}{\left({\frac {\ell }{r}}\right)^{2}}}$

where $F/A=\sigma$ is the stress that causes buckling the column, and $l/r$ is the slenderness ratio.

Since structural columns are commonly of intermediate length, the Euler formula has little practical application for ordinary design. Issues that cause deviation from the pure Euler column behaviour include imperfections in geometry of the column in combination with plasticity/non-linear stress strain behaviour of the column's material. Consequently, a number of empirical column formulae have been developed that agree with test data, all of which embody the slenderness ratio. Due to the uncertainty in the behavior of columns, for design, appropriate safety factors are introduced into these formulae. One such formula is the Perry Robertson formula which estimates the critical buckling load based on an assumed small initial curvature, hence an eccentricity of the axial load. The Rankine Gordon formula (Named for William John Macquorn Rankine and Perry Hugesworth Gordon (1899 – 1966)) is also based on experimental results and suggests that a column will buckle at a load F_max given by:

${\frac {1}{F_{\text{max}}}}={\frac {1}{F_{e}}}+{\frac {1}{F_{c}}}$

where F_e is the Euler maximum load and F_c is the maximum compressive load. This formula typically produces a conservative estimate of F_max.

Self-buckling

To get the mathematical demonstration read: Self-buckling

A free-standing, vertical column, with density $\rho$, Young's modulus $E$, and cross-sectional area $A$, will buckle under its own weight if its height exceeds a certain critical value:

$h_{crit}=\left({\frac {9B^{2}}{4}}\,{\frac {EI}{\rho gA}}\right)^{\frac {1}{3}}$

where g is the acceleration due to gravity, I is the second moment of area of the beam cross section, and B is the first zero of the Bessel function of the first kind of order -1/3, which is equal to 1.86635086…

Buckling under tensile dead loading

Fig. 2: Elastic beam system showing buckling under tensile dead loading.

Usually buckling and instability are associated with compression, but buckling and instability can also occur in elastic structures subject to dead tensile load.

An example of a single-degree-of-freedom structure is shown in Fig. 2, where the critical load is also indicated. Another example involving flexure of a structure made up of beam elements governed by the equation of the Euler's elastica is shown in Fig.3. In both cases, there are no elements subject to compression. The instability and buckling in tension are related to the presence of the slider, the junction between the two rods, allowing only relative sliding between the connected pieces. Watch a movie for more details.

Constraints, curvature and multiple buckling

Fig. 3: A one-degree-of-freedom structure exhibiting a tensile (compressive) buckling load as related to the fact that the right end has to move along the circular profile labeled 'Ct' (labelled 'Cc').

Buckling of an elastic structure strongly depends on the curvature of the constraints against which the ends of the structure are prescribed to move (see Bigoni, Misseroni, Noselli and Zaccaria, 2012). In fact, even a single-degree-of-freedom system (see Fig.3) may exhibit a tensile (or a compressive) buckling load as related to the fact that one end has to move along the circular profile labeled 'Ct' (labelled 'Cc').

Fig. 4: A one-degree-of-freedom structure with a 'S'-shaped bicircular profile exhibiting multiple bifurcations (both tensile and compressive).

The two circular profiles can be arranged in a 'S'-shaped profile, as shown in Fig.4; in that case a discontinuity of the constraint's curvature is introduced, leading to multiple bifurcations. Note that the single-degree-of-freedom structure shown in Fig.4 has two buckling loads (one tensile and one compressive). Watch a movie for more details.

Flutter instability

Structures subject to a follower (nonconservative) load may suffer instabilities which are not of the buckling type and therefore are not detectable with a static approach. For instance, the so-called 'Ziegler column' is shown in Fig.5.

Fig. 5: A sketch of the 'Ziegler column', a two-degree-of-freedom system subject to a follower load (the force P remains always parallel to the rod BC), exhibiting flutter and divergence instability. The two rods, of linear mass density ρ, are rigid and connected through two rotational springs of stiffness k1 and k2.

This two-degree-of-freedom system does not display a quasi-static buckling, but becomes dynamically unstable. To see this, we note that the equations of motion are

${\begin{aligned}{\frac {1}{3}}\rho l_{1}^{2}\left(l_{1}+3l_{2}\right){\ddot {\alpha }}_{1}+{\frac {1}{2}}\rho l_{1}l_{2}^{2}\cos(\alpha _{1}-\alpha _{2}){\ddot {\alpha }}_{2}+{\frac {1}{2}}\rho l_{1}l_{2}^{2}\sin(\alpha _{1}-\alpha _{2}){\dot {\alpha }}_{2}^{2}+{}&\\(k_{1}+k_{2})\alpha _{1}-k_{2}\alpha _{2}+(\beta _{1}+\beta _{2}){\dot {\alpha }}_{1}-\beta _{2}{\dot {\alpha }}_{2}-l_{1}P\sin(\alpha _{1}-\alpha _{2})&=0,\\[6pt]{\frac {1}{2}}\rho l_{1}l_{2}^{2}\cos(\alpha _{1}-\alpha _{2}){\ddot {\alpha }}_{1}+{\frac {1}{3}}\rho l_{2}^{3}{\ddot {\alpha }}_{2}-{\frac {1}{2}}\rho l_{1}l_{2}^{2}\sin(\alpha _{1}-\alpha _{2}){\dot {\alpha }}_{1}^{2}-{}&\\k_{2}(\alpha _{1}-\alpha _{2})-\beta _{2}({\dot {\alpha }}_{1}-{\dot {\alpha }}_{2})&=0,\end{aligned}}$

and their linearized version is

${\begin{aligned}{\frac {1}{3}}\rho l_{1}^{2}\left(l_{1}+3l_{2}\right){\ddot {\alpha }}_{1}+{\frac {1}{2}}\rho l_{1}l_{2}^{2}{\ddot {\alpha }}_{2}+(k_{1}+k_{2})\alpha _{1}-k_{2}\alpha _{2}-l_{1}P(\alpha _{1}-\alpha _{2})&=0,\\{\frac {1}{2}}\rho l_{1}l_{2}^{2}{\ddot {\alpha }}_{1}+{\frac {1}{3}}\rho l_{2}^{3}{\ddot {\alpha }}_{2}-k_{2}(\alpha _{1}-\alpha _{2})&=0.\end{aligned}}$

Assuming a time-harmonic solution in the form

$\alpha _{j}=A_{j}\,e^{-i\Omega \,t},~~~j=1,2,$

we find the critical loads for flutter ($\ P_{f}$) and divergence ($\ P_{d}$),

$P_{f,d}={\frac {k_{2}}{l_{1}}}\cdot {\frac {k+(1+\lambda )^{3}\mp \lambda \,{\sqrt {k(3+4\lambda )}}}{1+{\frac {3}{2}}\lambda }}$

where $\lambda =l_{1}/l_{2}$ and $k=k_{1}/k_{2}$.

Fig. 6: A sequence of deformed shapes at consecutive times intervals of the structure sketched in Fig.5 and exhibiting flutter (upper part) and divergence (lower part) instability.

Flutter instability corresponds to a vibrational motion of increasing amplitude and is shown in Fig.6 (upper part) together with the divergence instability (lower part) consisting in an exponential growth.

Recently, Bigoni and Noselli (2011) have experimentally shown that flutter and divergence instabilities can be directly related to dry friction, watch the movie for more details.

Various forms of buckling

Buckling is a state which defines a point where an equilibrium configuration becomes unstable under a parametric change of load and can manifest itself in several different phenomena. All can be classified as forms of bifurcation.

There are four basic forms of bifurcation associated with loss of structural stability or buckling in the case of structures with a single degree of freedom. These comprise two types of pitchfork bifurcation, one saddle-node bifurcation (often referred to as a limit point) and one transcritical bifurcation. The pitchfork bifurcations are the most commonly studied forms and include the buckling of columns, sometimes known as Euler buckling; the buckling of plates, sometimes known as local buckling, which is well known to be relatively safe (both are supercritical phenomena) and the buckling of shells, which is well-known to be a highly dangerous (subcritical phenomenon). Using the concept of potential energy, equilibrium is defined as a stationary point with respect to the degree(s) of freedom of the structure. We can then determine whether the equilibrium is stable, as in the case where the stationary point is a local minimum; or unstable, as in the case where the stationary point is a maximum point of inflection or saddle point (for multiple-degree-of-freedom structures only) – see animations below.

Archetypal rigid link models with a single degree of freedom (SDOF) used to demonstrate basic buckling phenomena (see bifurcation diagrams below). All cases start at the position corresponding to q=0.
Truss with spring tie (model shallow tied arch).  Link-strut with rotational spring.  Link-strut with transverse translational spring.  Asymmetrically supported link-strut.

Animations of the variation of total potential energy (red) for various load values, P (black), in generic structural systems with the indicated bifurcation or buckling behaviour.
Two saddle-node bifurcations (limit points).  Supercritical pitchfork bifurcation (stable-symmetric buckling point).  Subcritical pitchfork bifurcation (unstable-symmetric buckling point).  Transcritical bifurcation (asymmetric buckling point).

In Euler buckling, when the applied load is increased by a small amount beyond the critical load, the structure deforms into a buckled configuration which is adjacent to the original configuration. For example, the Euler column pictured will start to bow when loaded slightly above its critical load, but will not suddenly collapse.

In structures experiencing limit point instability, if the load is increased infinitesimally beyond the critical load, the structure undergoes a large deformation into a different stable configuration which is not adjacent to the original configuration. An example of this type of buckling is a toggle frame (pictured) which 'snaps' into its buckled configuration.

Bicycle wheels

A conventional bicycle wheel consists of a thin rim kept under high compressive stress by the (roughly normal) inward pull of a large number of spokes. It can be considered as a loaded column that has been bent into a circle. If spoke tension is increased beyond a safe level, the wheel spontaneously fails into a characteristic saddle shape (sometimes called a "taco" or a "pringle") like a three-dimensional Euler column. This is normally a purely elastic deformation and the rim will resume its proper plane shape if spoke tension is reduced slightly.

Surface materials

Railway tracks in the Netherlands affected by Sun kink.

Buckling is also a failure mode in pavement materials, primarily with concrete, since asphalt is more flexible. Radiant heat from the sun is absorbed in the road surface, causing it to expand, forcing adjacent pieces to push against each other. If the stress is great enough, the pavement can lift up and crack without warning. Going over a buckled section can be very jarring to automobile drivers, described as running over a speed hump at highway speeds.

Similarly, rail tracks also expand when heated, and can fail by buckling, a phenomenon called sun kink. It is more common for rails to move laterally, often pulling the underlain railroad ties (sleepers) along.

Cause

The buckling force in the track due to warming up is a function of the rise in temperature only and is independent of the track length:

$F=EA\alpha _{L}\Delta T$.

Derivation of buckling force function:

The linear thermal expansion due to heating of the track is found using

${\Delta L}=\alpha _{L}\Delta T\ L$

where

• ΔL = thermal expansion of the rail
• L = length of the rail/track
• α = coefficient of thermal expansion
• ΔT = increase in temperature

According to Hooke's law the extension due to a force (in the rail) is

$\Delta L={\frac {F}{EA}}L$

where

• ΔL = extension of the rail/track
• F = the force extending a rod, here the induced force in the rail
• E = modulus of elasticity of rail material (steel)
• A = cross section of rail
• L = length of rail

Putting these together gives

${\begin{aligned}{{\frac {F}{EA}}L}&=\alpha _{L}\Delta T\ L\Longleftrightarrow \\F&=EA\alpha _{L}\Delta T\end{aligned}}$

Accidents

These accidents were deemed to be sun kink related (more information available at List of rail accidents (2000–2009)):

• April 18, 2002 Amtrak Auto-Train derailment, off CSX tracks, near Crescent City, Florida.
• July 29, 2002 Amtrak Capitol Limited derails, off CSX tracks, near Kensington, Maryland.
• July 8, 2010 CSX train derails off tracks in Waxhaw, North Carolina.
• July 6, 2012 WMATA Metrorail train derails off tracks near Hyattsville, Maryland.

Energy method

Often it is very difficult to determine the exact buckling load in complex structures using the Euler formula, due to the difficulty in determining the constant K. Therefore, maximum buckling load is often approximated using energy conservation and referred to as an energy method in structural analysis.

The first step in this method is to assume a displacement mode and a function that represents that displacement. This function must satisfy the most important boundary conditions, such as displacement and rotation. The more accurate the displacement function, the more accurate the result.

The method assumes that the system (the column) is a conservative system in which energy is not dissipated as heat, hence the energy added to the column by the applied external forces is stored in the column in the form of strain energy.

$U_{\text{applied}}=U_{\text{strain}}\,$

In this method, there are two equations used (for small deformations) to approximate the "strain" energy (the potential energy stored as elastic deformation of the structure) and "applied" energy (the work done on the system by external forces).

${\begin{aligned}U_{\text{strain}}&={\frac {E}{2}}\int I(x)(w_{xx}(x))^{2}\,dx\\U_{\text{applied}}&={\frac {P_{\text{crit}}}{2}}\int (w_{x}(x))^{2}\,dx\end{aligned}}$

where $w(x)$ is the displacement function and the subscripts $x$ and $xx$ refer to the first and second derivatives of the displacement. Energy conservation yields:

Flexural-torsional buckling

Flexural-torsional buckling can be described as a combination of bending and twisting response of a member in compression. Such a deflection mode must be considered for design purposes. This mostly occurs in columns with "open" cross-sections and hence have a low torsional stiffness, such as channels, structural tees, double-angle shapes, and equal-leg single angles. Circular cross sections do not experience such a mode of bucking.

Lateral-torsional buckling

Lateral-torsional buckling of an I-beam with vertical force in center: a) longitudinal view, b) cross section near support, c) cross section in center with lateral-torsional buckling

When a simply supported beam is loaded in flexure, the top side is in compression, and the bottom side is in tension. If the beam is not supported in the lateral direction (i.e., perpendicular to the plane of bending), and the flexural load increases to a critical limit, the beam will experience a lateral deflection of the compression flange. The lateral deflection of the compression flange is restrained by the beam web and tension flange, but for an open section the twisting mode is more flexible, hence the beam both twists and deflects laterally in a failure mode known as lateral-torsional buckling. In wide-flange sections (with high lateral bending stiffness), the deflection mode will be mostly twisting in torsion. In narrow-flange sections, the bending stiffness is lower and the column's deflection will be closer to that of lateral bucking deflection mode.

The modification factor (C_b)

C_b is a modification factor used in the equation for nominal flexural strength when determining lateral-torsional buckling. The reason for this factor is to allow for non-uniform moment diagrams when the ends of a beam segment are braced. The conservative value for C_b can be taken as 1, regardless of beam configuration or loading, but in some cases it may be excessively conservative. C_b is always equal to or greater than 1, never less. For cantilevers or overhangs where the free end is unbraced, C_b is equal to 1. Tables of values of C_b for simply supported beams exist.

If an appropriate value of C_b is not given in tables, it can be obtained via the following formula:

$\ C_{b}={\frac {12.5M_{\max }}{2.5M_{\max }+3M_{A}+4M_{B}+3M_{C}}}$

where

$M_{\max }$ = absolute value of maximum moment in the unbraced segment,

$M_{A}$ = absolute value of maximum moment at quarter point of the unbraced segment,

$M_{B}$ = absolute value of maximum moment at centerline of the unbraced segment,

$M_{C}$ = absolute value of maximum moment at three-quarter point of the unbraced segment,

The result is the same for all unit systems.

Plastic buckling

The buckling strength of a member is less than the elastic buckling strength of a structure if the material of the member is stressed beyond the elastic material range and into the non-linear (plastic) material behavior range. When the compression load is near the buckling load, the structure will bend significantly and the material of the column will diverge from a linear stress-strain behavior. The stress-strain behavior of materials is not strictly linear even below the yield point, hence the modulus of elasticity decreases as stress increases, and significantly so as the stresses approach the material's yield strength. This reduced material rigidity reduces the buckling strength of the structure and results in a bucking load less than that predicted by the assumption of linear elastic behavior.

A more accurate approximation of the buckling load can be had by the use of the tangent modulus of elasticity, E_t, which is less than the elastic modulus, in place of the elastic modulus of elasticity. The tangent is equal to the elastic modulus and then decreases beyond the proportional limit. The tangent modulus is a line drawn tangent to the stress-strain curve at a particular value of strain (in the elastic section of the stress-strain curve, the tangent modulus is equal to the elastic modulus). Plots of the tangent modulus of elasticity for a variety of materials are available in standard references.

Dynamic buckling

If a column is loaded suddenly and then the load released, the column can sustain a much higher load than its static (slowly applied) buckling load. This can happen in a long, unsupported column used as a drop hammer. The duration of compression at the impact end is the time required for a stress wave to travel along the column to the other (free) end and back down as a relief wave. Maximum buckling occurs near the impact end at a wavelength much shorter than the length of the rod, and at a stress many times the buckling stress of a statically-loaded column. The critical condition for buckling amplitude to remain less than about 25 times the effective rod straightness imperfection at the buckle wavelength is

$\sigma L=\rho c^{2}h\,$

where $\sigma$ is the impact stress, $L$ is the length of the rod, $c$ is the elastic wave speed, and $h$ is the smaller lateral dimension of a rectangular rod. Because the buckle wavelength depends only on $\sigma$ and $h$, this same formula holds for thin cylindrical shells of thickness $h$.

Buckling of thin cylindrical shells subject to axial loads

Solutions of Donnell's eight order differential equation gives the various buckling modes of a thin cylinder under compression. But this analysis, which is in accordance with the small deflection theory gives much higher values than shown from experiments. So it is customary to find the critical buckling load for various structures which are cylindrical in shape from empirically based design curves wherein the critical buckling load F_cr is plotted against the ratio R/t, where R is the radius and t is the thickness of the cylinder for various values of L/R, L the length of the cylinder. If cut-outs are present in the cylinder, critical buckling loads as well as pre-buckling modes will be affected. Presence or absence of reinforcements of cut-outs will also affect the buckling load.

Buckling of pipes and pressure vessels subject to external overpressure

Pipes and pressure vessels subject to external overpressure, caused for example by steam cooling within the pipe and condensing into water with subsequent massive pressure drop, risk buckling due to compressive hoop stresses. Design rules for calculation of the required wall thickness or reinforcement rings are given in various piping and pressure vessel codes.

Cerebral cortex

The mechanisms of cortical gyrification are just beginning to be understood. Mechanical buckling forces due to the expanding brain tissue probably cause the cortical surface to fold.

See also

• Euler's critical load
• Perry Robertson formula
• Rail stressing
• Stiffening
• Wood method
• Yoshimura buckling

References

Further reading

• Timoshenko, S. P., and Gere, J. M., Theory of Elastic Stability, 2 ed., McGraw-Hill, 1961.
• Nenezich, M., Thermoplastic Continuum Mechanics, Journal of Aerospace Structures, Vol. 4, 2004.
• The Stability of Elastic Equilibrium by W. T. Koiter, PhD Thesis, 1945.
• Dhakal Rajesh and Koichi Maekawa (October 2002). "Reinforcement Stability and Fracture of Cover Concrete in Reinforced Concrete Members”. [1]
• Willian T. Segui (2007). “Steel Design” Fourth Edition. United States. Chris Carson.
• Analysis and design of flight vehicle structures- E.F.Bruhn

External links

• The complete theory and example experimental results for long columns are available as a 39-page PDF document at http://lindberglce.com/tech/buklbook.htm
• Laboratory for Physical Modeling of Structures and Photoelasticity (University of Trento, Italy)
• https://web.archive.org/web/20100401042249/http://www.midasuser.com.tw:80/t_support/tech_pds/files/Tech%20Note-Lateral%20Torsional%20Buckling.pdf

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• PMID 24163093

• 3-D ultrastructure and collagen composition of healthy and overloaded human tendon: evidence of tenocyte and matrix buckling.

• Pingel J1, Lu Y, Starborg T, Fredberg U, Langberg H, Nedergaard A, Weis M, Eyre D, Kjaer M, Kadler KE.Author information 1Faculty of Health and Medical Sciences, Institute of Sports Medicine, Bispebjerg Hospital and Centre for Healthy Aging, University of Copenhagen, Copenhagen, Denmark.AbstractAchilles tendinopathies display focal tissue thickening with pain and ultrasonography changes. Whilst complete rupture might be expected to induce changes in tissue organization and protein composition, little is known about the consequences of non-rupture-associated tendinopathies, especially with regards to changes in the content of collagen type I and III (the major collagens in tendon), and changes in tendon fibroblast (tenocyte) shape and organization of the extracellular matrix (ECM). To gain new insights, we took biopsies from the tendinopathic region and flanking healthy region of Achilles tendons of six individuals with clinically diagnosed tendinopathy who had no evidence of cholesterol, uric acid and amyloid accumulation. Biochemical analyses of collagen III/I ratio were performed on all six individuals, and electron microscope analysis using transmission electron microscopy and serial block face-scanning electron microscopy were made on two individuals. In the tendinopathic regions, compared with the flanking healthy tissue, we observed: (i) an increase in the ratio of collagen III : I proteins; (ii) buckling of the collagen fascicles in the ECM; (iii) buckling of tenocytes and their nuclei; and (iv) an increase in the ratio of small-diameter : large-diameter collagen fibrils. In summary, load-induced non-rupture tendinopathy in humans is associated with localized biochemical changes, a shift from large- to small-diameter fibrils, buckling of the tendon ECM, and buckling of the cells and their nuclei.
• Journal of anatomy.J Anat.2014 May;224(5):548-55. doi: 10.1111/joa.12164. Epub 2014 Feb 9.
• Achilles tendinopathies display focal tissue thickening with pain and ultrasonography changes. Whilst complete rupture might be expected to induce changes in tissue organization and protein composition, little is known about the consequences of non-rupture-associated tendinopathies, especially with
• PMID 24571576

Japanese Journal

• 米沢市立病院における裂孔原性網膜剝離に対する初回硝子体手術と強膜バックルの比較 (特集 第68回日本臨床眼科学会講演集(6))

• 髙宮 美智子,佐藤 憲夫,平田 勲 [他]
• 臨床眼科 69(8), 1219-1223, 2015-08
• NAID 40020541677

• 異種鋼材を併用した偏心座屈ブレースの提案とその実験的検証

• 稲益 博行,䔥 博謙,林 和宏 [他]
• 日本建築学会構造系論文集 80(713), 1165-1174, 2015-07
• NAID 40020530779

• せん断パネルダンパーの設計式に関する一考察 その4 スチフナ付せん断パネルダンパーのせん断載荷実験

• 玉井 宏章,妹尾 文貴,三久保 里弥
• 長崎大学大学院工学研究科研究報告 45(85), 15-20, 2015-07
• … Then, within this experimental range, with respect to the panel with stiffeners, by the panle buckling prediction region, it can better determine the presence or absence of pinching occurs. …
• NAID 120005619674

Related Links

• bucklingの意味・使い方・読み方｜英辞郎 on the WEB

buckling. 【名】. バックリング、座屈｛ざくつ｝. ＝ bloater. 【発音】bʌ́kliŋ、【＠】バクリング、【分節】buck・ling. bucklinganalyses. 座屈解析｛ざくつ かいせき｝ 「分析・解析」の単数形＝analysis、複数形＝analyses. 【表現パターン】buckling analysis [analyses] bucklingapproximation.

• buckling（バックリング）の意味 - goo国語辞書

buckling（バックリング）とは。意味や解説、類語。軸の長手方向に荷重をかけたとき、荷重と直角方向に生じる変形。 - goo国語辞書は30万3千件語以上を収録。政治・経済・医学・ITなど、最新用語の追加も定期的に行っています。

• 座屈 （読み）ざくつ （英語表記）buckling

座屈 （読み）ざくつ （英語表記）buckling

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★リンクテーブル★

リンク元	「ボウイング」「膝折れ」

「ボウイング」

　　[★]

英

bowing

同

バックリング buckling

「膝折れ」

　　[★]

英

buckling

関

膝くずれ