Torsion of Thin-walled Rectangular Bar | Online Calculator

Torsion of Bars Calculators







Torsion of Thin-walled Bar of Rectangular Cross Section

In this calculation, a rectangular thin walled bar of length L with the cross-sectional dimensions a × b and wall thicknesses s1 and s is considered.

The bar is under torque T, applied to the end. Following the calculations, the total twist angle φ and the maximum shear stresses τ in the section are determined.

For the calculation, the elastic modulus E and Poisson's ratio ν of the bar should be specified.

Thin walled bar of rectangular section under torsion
Calculation of Thin walled bar of rectangular section under torsion

INITIAL DATA

a - Cross-section width;


b - Cross-section height;


s - Wall thickness on "b" side;


s1 - Wall thickness on "a" side;


L - Bar length;


Т - Torque;


ν - Poisson's ratio;


Е - Young's modulus.

RESULTS DATA

τ - Maximum shear stress in the cross-section on "b" side;


τ1 - Maximum shear stress in the cross-section on "a" side;


φ - Twist angle.

Width (a)

Height (b)

Thickness (s)

Thickness (s1)

Bar length (L)

Torque (Т)

Poisson's ratio (ν)

Young's modulus (Е)

Shear stress (τ)

Shear stress (τ1)

Twist angle (φ)

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BASIC FORMULAS

Shear stress and twist angle are determined by parametric equations of the form:

τ = T / 2s(a - s)(b - s1);

τ1 = T / 2s1(a - s)(b - s1);

φ = TL / K1G;

G - Shear modulus;

K1 - coefficient, depending on dimensions of the rectangle.

INITIAL DATA

a - Cross-section width;


b - Cross-section height;


s - Wall thickness on "b" side;


s1 - Wall thickness on "a" side;


L - Bar length;


Т - Torque;


ν - Poisson's ratio;


Е - Young's modulus.

RESULTS DATA

τ - Maximum shear stress in the cross-section on "b" side;


τ1 - Maximum shear stress in the cross-section on "a" side;


φ - Twist angle.

MATERIALS PROPERTIES

Material

Young’s modulus

Pa (psi)

Poisson’s ratio

Steel

1.86÷2.1×1011 (2.7÷3.05×107)

0.25÷0.33

Cast iron

0.78÷1.47×1011 (1.1÷2.1×107)

0.23÷0.27

Copper

1.0÷1.3×1011 (1.45÷1.9×107)

0.34

Tin bronze

0.74÷1.22×1011 (1.1÷1.8×107)

0.32÷0.35

Brass

0.98÷1.08×1011 (1.4÷1.6×107)

0.32÷0.34

Aluminum alloy

0.7×1011 (1.0×107)

0.33

Magnesium alloy

0.4÷0.44×1011 (5.8÷6.4×106)

0.34

Nickel

2.5×1011 (3.6×107)

0.33

Titanium

1.16×1011 (1.7×107)

0.32

Lead

0.15÷0.2×1011 (2.2÷2.9×106)

0.42

Zinc

0.78×1011 (1.1×107)

0.27

Glass

4.9÷5.9×1010 (7.1÷8.5×106)

0.24÷0.27

Concrete

1.48÷2.25×1010 (2.1÷3.3×106)

0.16÷0.18

Wood (along the grain)

8.8÷15.7×1010 (12.8÷22.8×106)

-

Wood (across the grain)

3.9÷9.8×1010 (5.7÷14.2×106)

-

Nylon

1.03×1010 (1.5×106)

-

OTHER CALCULATORS

AREA MOMENTS OF INERTIA
BEAM CALCULATORS
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CIRCULAR FLAT PLATES
BUCKLING
ELASTIC CONTACT
IMPACT LOADS
NATURAL FREQUENCIES
PRESSURED SHELLS
FLUID DYNAMIC
COMPOSITES
SPRINGS
THREAD CONNECTIONS
SHAFT CONNECTIONS
BEARINGS
DRIVES
FATIGUE
HEAT TRANSFER