Online calculator for determining the permissible stresses of materials: steels and alloys of aluminum, copper and titanium.

The online calculator determines the calculated permissible stresses σ depending on the design temperature for various grades of materials of the following types: carbon steel, chromium steel, austenitic steel, austenitic-ferritic steel, aluminum and its alloys, copper and its alloys, titanium and its alloys according GOST-52857.1-2007 [1].

Initial data:
Estimated ambient temperature T, °C
Material type
Material grade
Solution:
Allowable stress of the material [σ], MPadetermination of permissible stress

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I. Calculation method:

Allowable stresses were determined according to GOST-52857.1-2007 [1].

for carbon and low alloy steels

St3, 09G2S, 16GS, 20, 20K, 10, 10G2, 09G2, 17GS, 17G1S, 10G2S1:

  1. At design temperatures below 20°C, the permissible stresses are taken to be the same as at 20°C, subject to the permissible use of the material at a given temperature.
  2. For intermediate design wall temperatures, the permissible stress is determined by linear interpolation with rounding the results down to 0.5 MPa.
  3. For steel grade 20 at Re/20e/20/220.
  4. For steel grade 10G2 at Rр0.2/20р0.2/20/270.
  5. For steel grades 09G2S, 16GS, strength classes 265 and 296 according to GOST 19281, the permissible stresses, regardless of the sheet thickness, are determined for thicknesses over 32 mm.
  6. The permissible stresses located below the horizontal line are valid for a service life of no more than 105 hours. For a design service life of up to 2*105 hours, the permissible stress located below the horizontal line is multiplied by the coefficient: for carbon steel by 0.8; for manganese steel by 0.85 at temperatures <450 °C and by 0.8 at temperatures from 450 °C to 500 °C inclusive.

Allowable stresses for carbon steels of ordinary quality in the hot-rolled state

table 1

Steel grade according to GOST 380Allowable stress, kgf/cm2
When stretched
[σр]
When bending
[σ from]
In torsion
[τ cr]
When cutting
[τ avg]
When crushed
[σ cm]
IIIIIIIIIIIIIIIIIIIIIIIIIII
St 211508006001400100080085065050070050040017501200
St. 312509007001500110085095065050075050040019001350
St. 4140095075017001200950105075060085065050021001450
St. 5165011509002000140011001250900700100065055025001750
St. 619501400110023001700135014501050800115085065029002100

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for heat-resistant chromium steels

12XM, 12MX, 15XM, 15X5M, 15X5M-U:

  1. At design temperatures below 20 °C, the permissible stresses are taken to be the same as at 20 °C, subject to the permissible use of the material at a given temperature.
  2. For intermediate design wall temperatures, the permissible stress is determined by linear interpolation with rounding the results down to 0.5 MPa.
  3. The permissible stresses located below the horizontal line are valid for a service life of 105 hours. For a design service life of up to 2 * 105 hours, the permissible stress located below the horizontal line is multiplied by a factor of 0.85.

Types of tensile strength

Tensile strength is one of the main mechanical parameters of steel, as well as any other structural material.

This value is used in strength calculations of parts and structures; based on it, it is decided whether a given material is applicable in a particular area or whether a more durable one needs to be selected.

The following types of tensile strength are distinguished:

  • compression - determines the ability of a material to resist the pressure of an external force;
  • bending - affects the flexibility of parts;
  • torsion - shows how suitable the material is for loaded drive shafts that transmit torque;
  • stretching

Types of material strength tests

The scientific name for the parameter used in standards and other official documents is tensile strength.

for heat-resistant, heat-resistant and corrosion-resistant austenitic steels

03X21H21M4GB, 03X18H11, 03X17H14M3, 08X18H10T, 08X18H12T, 08X17H13M2T, 08X17H15M3T, 12X18H10T, 12X18H12T, 10X17H13M2T, 10X 17H13M3T, 10X14G14H4:

  1. At design temperatures below 20 °C, the permissible stresses are taken to be the same as at 20 °C, subject to the permissible use of the material at a given temperature.
  2. For intermediate design wall temperatures, the permissible stress is determined by interpolating the two closest values ​​​​indicated in the table, with the results rounded down to the nearest 0.5 MPa.
  3. For forgings made of steel grades 12Х18Н10Т, 10Х17Н13M2T, 10Х17Н13М3Т, the permissible stresses at temperatures up to 550 °C are multiplied by 0.83.
  4. For long rolled steel grades 12Х18Н10Т, 10Х17Н13M2T, 10Х17Н13М3Т, permissible stresses at temperatures up to 550 °С are multiplied by the ratio (R*p0.2/20) / 240. (R*p0.2/20 - the yield strength of the long rolled material is determined by GOST 5949).
  5. For forgings and long products made of steel grade 08X18H10T, the permissible stresses at temperatures up to 550 °C are multiplied by 0.95.
  6. For forgings made of steel grade 03X17H14M3, the permissible stresses are multiplied by 0.9.
  7. For forgings made of steel grade 03X18H11, the permissible stresses are multiplied by 0.9; for long products made of steel grade 03X18H11, the permissible stresses are multiplied by 0.8.
  8. For pipes made of steel grade 03Х21Н21М4ГБ (ZI-35), the permissible stresses are multiplied by 0.88.
  9. For forgings made of steel grade 03Х21Н21М4ГБ (ZI-35), the permissible stresses are multiplied by the ratio (R*p0.2/20) / 250. (R*p0.2/20 is the yield strength of the forging material, determined according to GOST 25054).
  10. The permissible stresses located below the horizontal line are valid for a service life of no more than 105 hours.

For a design service life of up to 2*105 hours, the permissible voltage located below the horizontal line is multiplied by a factor of 0.9 at temperatures <600 °C and by a factor of 0.8 at temperatures from 600 °C to 700 °C inclusive.

Mechanical properties and permissible stresses of alloy structural steels

table 3

Steel grade GOST 1050GOSTHeat
treatment
Tensile strength σ inYield strength σ tEndurance limit atAllowable stresses *, kgf/cm2, at
stretching
σ −1р
bending σ −1torsion τ −1stretch
[σ р]
bending [σ out]torsion [τ cr]cut [τ avg]crushing [σ cm]
kgf/mm 2IIIIIIIIIIIIIIIIIIIIIIIIIII
10G24543N432517,52212,514001100900170013501100105075060085065050021001650
09G2S192825035192414170012009502000150012001250900700100070055025001800
10HSND19282544021,52715,518501400110022001600135014001000800110080065028002100
20X4543N603021261519001350105023001650130014001000750115085060028002000
U70502835202400175014002900220017501800130010001450105080036002600
M5985633442242900210017003500145021002200155012001750125095043003200
40XN633325311820001550125024001900155015001150900120095075030002300
U80653240232700200016003200250020002000150011501600115090040003000
M391109044553238002800220045003400270028002000160023001650130056004200
M4813011052653844003300260053004100320033002400190027001950150067004900
45XN6535263218,521001600130025001950160015501150900125095075031002400
U957538472732002400190038002900230024001750135019001350105048003600
M4814012056704048003500280057004300350036002600200029002000160072005200
50XN65352632,518,521001600130025002000160016001200900125090070031002400
M4815013060754350003700300060004600370037002700210030002200170075005500
35G2N63372531,51820001550125024001900160015001150900120095075033002300
B, HB24980653240232700200016003200250020002000145011501600115090040003000
40G2N67392733,519,522001700135026002100170016501200950130095075033002500
M, NV3311129554663838003100270046003800330029002300190023001900150058004600
45G2N70412835202300175014002700210017501750125010001400100080034002600
M, NV29585703442,524,52900210017003500145021002200155012001750125095044003300
33ХСN603021261519001350105023001650130014001000750115065060028002000
M907036452630002200180036002800220023001650130018001350105045003300
38ХСU957537472832002300185039002900230024001750140019001400110048003500
18ХГТN70432835202300175014002700210017501700125010001400100080034002600
Ts-M591008040502933002500200040003100250025001850145020001450115049003800
30ХГТM4312510550623643003100250051003900310032002300180026001850140064004600
Ts-M591108044553237002700220044003400270028002000160022001600125055004100
20ХГНРM40130120526537,545003300260054004100320034002300170027001800135068005000
M501451405872,54250003600290060004500360038002700210030002150170075005400
40HFAM30907536452632002300180038002800220024001700130019001350105048003400
M5016013064804855004100320066005000400041003100240033002400195082006100
30ХМM95753847,5233200240019003900300024002400155011501900125090048003600
35ХМM, HB270100854050293400250020004100310025002600185014502000130095052003800
M5016014064804855004100320066005000400042003100240033002500200082006100
40ХНN7846313922,52600195016003100240019501900140011001550115090039002900
M43120100486034,541003100240049003700300031002200170025001750135062004600
12ХН2M80603240232700200016003200250020002000145011501600115090040003000
Ts-M5980603240232700200016003200250020002000145011501600115090040003000
12ХН3АU957038472732002400190038002800230024001750140019001400110048003000
TVCh591008540503034002600200041003100250025001900150020001500120051003800
20Х2Н4АTVCh5968452734202300170013502700210017001700125010001400100080034002600
Ts-M591108544553237002700220044003400270028002000160022001600125055004100
M130110526537,544003300260053004000320033002400190026001900150066005000
20ХГСАM80653240232700200016003300250020002000145011501600115090041003000
30ХГСABOUT603624301720001500120024001850150015001100850120090070030002200
30ХГСАU1108544553237002700220044003400270028002000160022001600125055004100
M4615013060754351003800300062004700380039002700210031002200170076005700
38Х210M80703240232800200016003300250020002000150011501700120095041003000
M907536452631002400190037002900240023001700135018501400110046003600
50HFA14959M13011052653444003300260054004000320034002200170026001800135066005000
M4615013060753652003800300062004700380039002400180031002000145077005700
60С2M, NV26913012052653444003300260054004000320034002200170026001800135067005000
60С2АM, NV269160140648046,555004000320066005000400041003000230033002400185082006000
ШХ15801ABOUT603824301820001500120024001800150015001100900120090075030002200
M62220170466633740035002300890048003300550025001650440020001300110005200

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for titanium and its alloys

VT1-0, OT4-0, AT3, VT1-00:

  1. At design temperatures below 20 °C, the permissible stresses are taken to be the same as at 20 °C, subject to the permissibility of using the material at a given temperature.
  2. For forgings and rods, the permissible stresses are multiplied by 0.8.

II. Definitions and notations:

Re/20 - minimum value of the yield strength at a temperature of 20 °C, MPa; Rр0.2/20 - minimum value of the conditional yield strength at a permanent elongation of 0.2% at a temperature of 20 °C, MPa. permissible stress - the highest stress that can be allowed in a structure, subject to its safe, reliable and durable operation. The value of the permissible stress is established by dividing the tensile strength, yield strength, etc. by a value greater than one, called the safety factor. design temperature - the temperature of the wall of equipment or a pipeline, equal to the maximum arithmetic mean value of the temperatures on its outer and inner surfaces in one section under normal operating conditions (for parts of nuclear reactor vessels, the design temperature is determined taking into account internal heat releases as the average integral value of the temperature distribution over the thickness of the vessel wall ( PNAE G-7-002-86, clause 2.2; PNAE G-7-008-89, appendix 1).

Design temperature

  • [1], clause 5.1. The design temperature is used to determine the physical and mechanical characteristics of the material and permissible stresses, as well as when calculating strength taking into account temperature effects.
  • [1], clause 5.2. The design temperature is determined on the basis of thermal calculations or test results, or operating experience of similar vessels.
  • The highest wall temperature is taken as the design temperature of the wall of the vessel or apparatus. At temperatures below 20 °C, a temperature of 20 °C is taken as the design temperature when determining permissible stresses.
  • [1], clause 5.3. If it is impossible to carry out thermal calculations or measurements and if during operation the wall temperature rises to the temperature of the medium in contact with the wall, then the highest temperature of the medium, but not lower than 20 °C, should be taken as the design temperature.
  • When heating with an open flame, exhaust gases or electric heaters, the design temperature is taken equal to the ambient temperature increased by 20 °C for closed heating and by 50 °C for direct heating, unless more accurate data are available.
  • [1], clause 5.4. If a vessel or apparatus is operated under several different loading modes or different elements of the apparatus operate under different conditions, for each mode its own design temperature can be determined (GOST-52857.1-2007, clause 5).

III. Note:

The source data block is highlighted in yellow, the intermediate calculation block is highlighted in blue, and the solution block is highlighted in green.

How is strength testing performed?

Strength tests for tensile strength are carried out on special test benches.
One end of the test sample is fixedly fixed in them, and a drive mount, electromechanical or hydraulic, is attached to the other. This drive creates a smoothly increasing force that acts to break the sample, or to bend or twist it. Tensile test

The electronic control system records the tensile force and relative elongation, and other types of deformation of the sample.

Harmful impurities

These primarily include: phosphorus,

which, forming a solution with ferrite, increases the brittleness of steel, especially at low temperatures (cold brittleness) and reduces ductility at elevated temperatures;

sulfur,

making steel red-brittle (prone to cracking at temperatures of 800 - 1000 C) due to the formation of low-melting iron sulfide. Therefore, the content of sulfur and phosphorus in steel is limited; So in carbon steel St 3, sulfur is up to 0.05% and phosphorus is up to 0.04%.

The mechanical properties of steel are adversely affected by saturation with gases that can enter the metal in a molten state from the atmosphere. Oxygen acts like sulfur, but to a greater extent and increases the brittleness of steel. Unfixed nitrogen also reduces the quality of steel. Hydrogen, although retained in an insignificant amount (0.0007%), but concentrating near inclusions in intercrystalline regions and located mainly along the boundaries of blocks, causes high stresses in microvolumes, which leads to a decrease in the resistance of steel, brittle fracture, a decrease in tensile strength and plastic properties become. Therefore, molten steel (for example during welding) must be protected from exposure to the atmosphere.

Proof of Yield

In addition to the tensile strength, the related concept of yield strength, denoted σt, is widely used in engineering calculations. It is equal to the amount of tensile strength that must be created in the material in order for the deformation to continue to increase without increasing the load. This state of the material immediately precedes its destruction.

At the microlevel, at such stresses, interatomic bonds in the crystal lattice begin to break, and the specific load on the remaining bonds increases.

Alloying additives in alloys

These are substances deliberately added to the melt to improve the properties of the alloy and bring its parameters to the required ones. Some of them are added in large quantities (more than a percent), others in very small quantities. I most often use the following alloying additives:

  • Chromium. Used to increase hardenability and hardness. Share - 0.8-0.2%.
  • Bor. Improves cold brittleness and radiation resistance. Share - 0.003%.
  • Titanium. Added to improve the structure of Cr-Mn alloys. Share - 0.1%.
  • Molybdenum. Increases strength characteristics and corrosion resistance, reduces fragility. Share - 0.15-0.45%.
  • Vanadium. Improves strength parameters and elasticity. Share - 0.1-0.3%.
  • Nickel. Promotes an increase in strength characteristics and hardenability, but at the same time leads to an increase in fragility. This effect is compensated by the simultaneous addition of molybdenum.

Metallurgists also use more complex combinations of alloying additives, achieving unique combinations of physical and mechanical properties of steel. The cost of such grades is several times (or even tens of times) higher than the cost of conventional low-carbon steels. They are used for particularly critical structures and assemblies.

Using the properties of metals

Two important indicators - plasticity and PP - are interrelated. Materials with a large first parameter degrade much more slowly. They change their shape well and are subjected to various types of metal processing, including die stamping - that’s why car body elements are made from sheets. With low ductility, alloys are called brittle. They can be very hard, but at the same time have poor stretching, bending and deformation, for example, titanium.

Resistance

There are two types:

  • Regulatory - prescribed for each type of steel in GOSTs.
  • Calculated – obtained after calculations in a specific project.

The first option is rather theoretical; the second is used for practical tasks.

Young's modulus of elasticity and shear, Poisson's ratio values ​​(Table)

Elastic properties of bodies

Below are reference tables for commonly used constants;
if two of them are known, then this is quite sufficient to determine the elastic properties of a homogeneous isotropic solid. Young's modulus or modulus of longitudinal elasticity in dyn/cm2.

Shear modulus or torsional modulus G in dyn/cm2.

Compressive modulus or bulk modulus K in dynes/cm2.

Poisson's ratio µ is equal to the ratio of transverse relative compression to longitudinal relative tension.

For a homogeneous isotropic solid material, the following relationships between these constants hold:

Poisson's ratio has a positive sign and its value is usually between 0.25 and 0.5, but in some cases it can go beyond these limits. The degree of agreement between the observed values ​​of µ and those calculated using formula (b) is an indicator of the isotropy of the material.

Tables of Young's Modulus of Elasticity, Shear Modulus and Poisson's Ratio

Values ​​calculated from relations (a), (b), (c) are given in italics.

Material at 18°CYoung's modulus E, 1011 dynes/cm2.Shear modulus G, 1011 dynes/cm2.Poisson's ratio µModulus of bulk elasticity K, 1011 dynes/cm2.
Aluminum7,052,620,3457,58
Bismuth3,191,200,3303,13
Iron21,28,20,2916,9
Gold7,82,70,4421,7
Cadmium4,991,920,3004,16
Copper12,984,8330,34313,76
Nickel20,47,90,28016,1
Platinum16,86,10,37722,8
Lead1,620,5620,4414,6
Silver8,273,030,36710,4
Titanium11,64,380,3210,7
Zinc9,03,60,256,0
Steel (1% C) 1)21,08,100,29316,88
(soft)21,08,120,29116,78
Constantan 2)16,36,110,32715,7
Manganin12,44,650,33412,4
1) For steel containing about 1% C, elastic constants are known to change during heat treatment.

The experimental results given below are for common laboratory materials, mainly wires.

SubstanceYoung's modulus E, 1011 dynes/cm2.Shear modulus G, 1011 dynes/cm2.Poisson's ratio µModulus of bulk elasticity K, 1011 dynes/cm2.
Bronze (66% Cu)-9,7-10,23,3-3,70,34-0,4011,2
Copper10,5-13,03,5-4,90,3413,8
Nickel silver1)11,64,3-4,70,37
Glass5,1-7,13,10,17-0,323,75
Glass yen crowns6,5-7,82,6-3,20,20-0,274,0-5,9
Jena flint glass5,0-6,02,0-2,50,22-0,263,6-3,8
Welding iron19-207,7-8,30,2916,9
Cast iron10-133,5-5,30,23-0,319,6
Magnesium4,251,630,30
Phosphor bronze2)12,04,360,38
Platinoid3)13,63,60,37
Quartz threads (floating)7,33,10,173,7
Soft vulcanized rubber0,00015-0,00050,00005-0,000150,46-0,49
Steel20-217,9-8,90,25-0,3316,8
Zinc8,73,80,21
1) 60% Cu, 15% Ni, 25% Zn 3) Nickel silver with a small amount of tungsten.
SubstanceYoung's modulus E, 1011 dynes/cm2.SubstanceYoung's modulus E, 1011 dynes/cm2.
Zinc (pure)9,0Oak1,3
Iridium52,0Pine0,9
Rhodium29,0Red tree0,88
Tantalum18,6Zirconium7,4
Invar17,6Titanium10,5-11,0
Alloy 90% Pt, 10% Ir21,0Calcium2,0-2,5
Duralumin7,1Lead0,7-1,6
Silk threads10,65Teak1,66
Web20,3Silver7,1-8,3
Catgut0,32Plastics:
Ice (-20C)0,28Thermoplastic0,14-0,28
Quartz7,3Thermoset0,35-1,1
Marble3,0-4,0Tungsten41,1
1) Reduces rapidly with increasing load 2) Detects noticeable elastic fatigue
Temperature coefficient (at 150C) Et=E11 (1-ɑ (t-15)), Gt=G11 (1-ɑ (t-15))Compressibility k, bar-1 (at 7-110C)
ɑ, for Eɑ, for G
Aluminum4,8*10-45,2*10-4Aluminum1,36*10-6
Brass3,7*10-44,6*10-4Copper0,73*10-6
Gold4,8*10-43,3*10-4Gold0,61*10-6
Iron2,3*10-42,8*10-4Lead2,1*10-6
Steel2,4*10-42,6*10-4Magnesium2,8*10-6
Platinum0,98*10-41,0*10-4Platinum0,36*10-6
Silver7,5*10-44,5*10-4Flint glass3,0*10-6
Tin5,9*10-4German glass2,57*10-6
Copper3,0*10-43,1*10-4Steel0,59*10-6
Nickel silver6,5*10-4
Phosphor bronze3,0*10-4
Quartz threads-1,5*10-4-1,1*10-4
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