Your Equation

Library / Structural dynamics and vibration testing / SDY-19

Structural dynamics and vibration testing

Longitudinal frequencies of a fixed–free rod

Axial (compression-wave) natural frequencies of a uniform slender rod fixed at one end and free at the other, from Young’s modulus E, density ρ, length L and the mode number n.

Ref
SDY-19
Rev
v1
Field
Structural dynamics and vibration testing
Result
fn [Hz]

A uniform slender rod with one end fixed and one end free vibrates axially at fₙ = (2n − 1)√(E/ρ)/(4L). The frequencies are the odd multiples of the fundamental. The wave speed in the rod is c = √(E/ρ), about 5000 m/s in steel. The result needs long wavelengths compared with the section size. E is entered in GPa.

Axial (compression-wave) natural frequencies of a uniform slender rod fixed at one end and free at the other, from Young’s modulus E, density ρ, length L and the mode number n.

Calculator

Solve for
Hz
18
GPa
1400
kg/m³
1,00020,000
m
0.55
  • Wave speed, √(E/ρ)5,000 m/s
  • Fundamental (n = 1)625 Hz
  • Wavelength of this mode, 4L/(2n − 1)2.667 m

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Axial natural frequency (Hz) current value 1,875 Hz
nMode numberKey driver
6259,380
LRod length
7507,500
ρDensity
1,1905,300
EYoung’s modulus
1332,650
  • Mode 2 of a 2 m rod vibrates axially at 1,875 Hz; the wave speed is 5,000 m/s.
  • Axial frequencies are far above bending frequencies for the same rod, which is why bending usually dominates the low-frequency response.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (Hz)Local stepChange in result
n Mode number1 to 8 6259,3758,750+1 +66.7 %
L Rod length0.5 to 5 m7507,5006,750+10%−9.09 %
ρ Density1,000 to 20,000 kg/m³1,1865,3034,117+10%−4.65 %
E Young’s modulus1 to 400 GPa132.62,6522,519+10%+4.88 %

Sweep of Rod length

Rod length (m)Axial natural frequency (Hz)
0.57,500
1.0633,529
1.6252,308
2.1881,714
2.751,364
3.3131,132
3.875967.7
4.438845.1
5750

Sweep one variable

Axial natural frequency (Hz)Hover, touch, or use the arrow keys on the chart
2000400060008000 12345 Rod length (m) now 1,875

Variables and how each one contributes

fn

Axial natural frequency

Result · Hz

What the equation gives you. Everything else feeds it.

n

Mode number

· typical 1 to 8

The mode or harmonic number (a whole number from 1). Raises the frequency in direct proportion (for the string) or in steps. Raising it by 1 (to 3) moves the result by +66.7 %, from 1,875 to 3,125 Hz.

E

Young’s modulus

GPa · typical 1 to 400

Young’s modulus, in GPa (steel about 200). A stiffer material raises the axial frequencies and the impedance. Raising it by 10 % (to 220) moves the result by +4.88 %, from 1,875 to 1,967 Hz.

ρ

Density

kg/m³ · typical 1,000 to 20,000

The density, in kg/m³ (steel about 7850). A denser material lowers the frequencies. Raising it by 10 % (to 8,800) moves the result by −4.65 %, from 1,875 to 1,788 Hz.

L

Rod length

m · typical 0.5 to 5

The span or length, in m. A longer span lowers the frequency. Raising it by 10 % (to 2.2) moves the result by −9.09 %, from 1,875 to 1,705 Hz.

Worked example with the values above

  1. Wave speed: √(E/ρ) = √(200 × 10⁹ / 8,000) = 5,000 m/s.
  2. Odd multiple over four lengths: (2n − 1)/(4L) = 3 / 8 = 0.375 1/m.
  3. fₙ = 1,875 Hz.

Assumptions and limits

  • Small motion, a uniform string, membrane or rod, and perfectly fixed or free ends as stated.
  • Negligible bending stiffness for strings and membranes, and long axial wavelengths compared with the rod section.

Common mistakes

  • Using tension in N for a membrane, which needs N/m, or the area mass in place of the mass per metre.
  • Using the string result for a stiff or thick wire, where bending stiffness raises the high harmonics.
  • Entering Young’s modulus in Pa when GPa is expected.

Statistics and uncertainty

Frequency follows the square root of tension or modulus over mass, and inversely with length, so length and mass are usually the dominant errors. Real supports are never perfectly fixed, which lowers measured frequencies.

Where it is used

  • Tuning and design of strings, cables, drum skins, diaphragms and axial rods.
  • Checking axial wave speeds and impedances at joints in impact and pile tests.

Maths you need

  • Wave speed: c = √(tension/mass per length), or √(E/ρ)
  • Standing waves: modes that fit the boundaries
  • Young’s modulus: stress over strain

Related formulas

Practise this formula