Sine Vibration Calculator: Convert Acceleration (g), Velocity and Displacement (Peak, RMS, Peak to Peak) at Any Frequency

Each row is one sine vibration point. Type any two of frequency, acceleration, velocity and displacement, and the row fills in the other two. Two amplitudes with no frequency give the crossover frequency where they are equal. Pick peak, rms or peak-to-peak and US or metric units at the top of each column.

Sine point converter

Points
Sine vibration points. Enter any two of frequency, acceleration, velocity and displacement in each row.
# Frequency
Hz
Acceleration Velocity Displacement Delete row
150.25563.1420.2
213.9928.7870.2
33323.7240.03592
452.1255.8950.036
550050.61450.0003912
typed calculated
Keyboard and paste
  • Tab moves along the row, then to the next row. Tab from the last cell adds a row.
  • Enter, ↓ and ↑ move down and up the same column, like a spreadsheet.
  • Calculated cells (grey italic) stay editable. Type over one and it becomes an input; the cell you typed least recently is calculated instead.
  • Ctrl+Delete removes the current row. Esc undoes the cell you are in.
  • Paste columns from Excel or a spec into any cell. They fill from that column to the right. 4x10^-2 and 4E-2 both work.
All units, row 1
At5 Hz
PeakRMSPeak to peak
Acceleration0.256 g2.51 m/s²0.181 g1.77 m/s²0.511 g5.01 m/s²
Velocity3.14 in/s79.8 mm/s2.22 in/s56.4 mm/s6.28 in/s160 mm/s
Displacement0.100 in2.54 mm0.0707 in1.80 mm0.200 in5.08 mm

Peak to peak displacement is the double amplitude (DA): 200 mils, 5,080 µm. ω = 2πf = 31.4 rad/s. One cycle takes 200 ms.

Click or tab into a row to show it here. For a sine wave, rms = peak ÷ √2 and peak to peak = 2 × peak.

Sine vibration nomograph

Acceleration vs frequency, with lines of constant displacement and velocity

Solid lines: constant displacement (rise 2 decades of g per decade of frequency). Dashed lines: constant velocity (1 decade per decade). The selected row is red. A sine sweep profile is a path along these lines: constant displacement at low frequency, then constant g.

Displacement and velocity for 1 g peak

Displacement falls with the square of frequency. Velocity falls in proportion to it. For any other g level, multiply the row by that level: 5 g at 20 Hz is 5 × 0.0489 = 0.245 in DA.

Frequency, HzDisplacement, in DADisplacement, mm pk-pkVelocity, in/s peakVelocity, mm/s peak
50.78219.912.3312
100.1964.976.14156
200.04891.243.0778.0
500.007820.1991.2331.2
1000.001960.04970.61415.6
2004.89×10⁻⁴0.01240.3077.80
5007.82×10⁻⁵0.001990.1233.12
10001.96×10⁻⁵4.97×10⁻⁴0.06141.56
20004.89×10⁻⁶1.24×10⁻⁴0.03070.780

MIL-STD-810H examples, checked

Figure 514.8E-2 (helicopter minimum integrity) is a sine sweep from 5 to 500 Hz: 0.20 in DA, then 2 g, then 0.036 in DA, then 5 g. Its corner frequencies are the crossovers between those levels. They are built into the converter as the default points, and the page's math gives the printed values.

MIL-STD-810H, Method 514.8InputsPrintedHere
Fig. 514.8E-2, first corner0.20 in DA meets 2 g14 Hz13.99 Hz
Fig. 514.8E-2, second corner2 g meets 0.036 in DA33 Hz32.96 Hz
Fig. 514.8E-2, third corner0.036 in DA meets 5 g52.1 Hz52.12 Hz
Fig. 514.8E-2, metric labels0.20 in and 0.036 in DA5.1 mm, 0.91 mm5.08 mm, 0.914 mm
Para. 4.1.2, loose cargo package tester25.4 mm (1.0 in) pk-pk at 5 Hznot printed1.28 g peak, 15.7 in/s peak
Reference Guide: Sine Vibration Units
01

Peak, RMS and Peak to Peak

Three ways to state one amplitude

Peak (also "single amplitude", "0-pk"): from the center to one extreme.

Peak to peak (also "double amplitude", DA, "pk-pk"): from one extreme to the other. It is 2 × peak.

RMS: the root mean square. For a pure sine wave it is peak ÷ √2, or 0.707 × peak.

A mil is 0.001 in. Displacement on rotating machinery is often given in mils pk-pk.

Which one specs use
QuantityUsual sine test convention
Accelerationg peak
Velocityin/s or mm/s peak; rms for machinery
Displacementin DA or mm pk-pk
The most common error is a factor of 2 between peak and DA displacement. Check which one a spec means before you set a shaker. MIL-STD-810H writes "double amplitude" in full.
02

The Formulas

One frequency, three amplitudes

With ω = 2πf and x the peak displacement, sine motion has peak velocity v = ω·x and peak acceleration a = ω·v = ω²·x.

In test units, with g = 386.09 in/s² = 9.80665 m/s²:

g = 0.0511 · f² · DA (DA in inches)
g = 0.00201 · f² · DA (DA in mm)
v = π · f · DA (peak velocity, same length unit per second)

Crossover frequency

Two amplitudes with no frequency meet at one frequency only. Solve the formulas above for f:

g and DA: f = √(g / (0.0511 · DA))
g and velocity: f = g · 386.09 / (2π · v)
velocity and DA: f = v / (π · DA)

Example: 2 g and 0.20 in DA cross at √(2 / (0.0511 × 0.20)) = 14.0 Hz, the first corner of MIL-STD-810H Figure 514.8E-2.
03

Why Sine Profiles Switch from Displacement to g

The same g needs far more stroke at low frequency

At 1 g, the table moves 0.78 in pk-pk at 5 Hz but only 0.002 in at 100 Hz. A constant-g profile would need a huge stroke at the low end, and a constant-displacement profile would need huge g at the high end.

So sine profiles hold displacement at low frequency and g at high frequency, joined at a crossover. Some add a constant-velocity band between them.

Shaker limits follow the same lines

An electrodynamic shaker is limited by stroke at low frequency, by velocity in the middle, and by force (g times moving mass) at high frequency. On the nomograph above those are a constant-displacement line, a constant-velocity line and a constant-g line.

Check every corner of a profile against the shaker's rated stroke (pk-pk), velocity (peak) and force. The test needs all three at once.
04

Sine g Is Not Random Grms

Everything on this page is for a single sine tone. The rms column is that tone's rms, peak ÷ √2.

A random test's Grms comes from the whole spectrum at once, and its peaks are about 3 × Grms. A random ASD value (g²/Hz) cannot be converted to a sine g point by point. Use the random vibration PSD calculator for random profiles.

05

Sources

MIL-STD-810H, Environmental Engineering Considerations and Laboratory Tests, Method 514.8 Vibration (31 January 2019; public release). Annex E, Figure 514.8E-2 (Category 24, helicopter minimum integrity exposure). Paragraph 4.1.2 (Procedure II, loose cargo transportation: 25.4 mm pk-pk at 5 Hz).

Standard gravity g = 9.80665 m/s² (exact, CGPM 1901); 1 in = 25.4 mm (exact).

The conversions are the equations of simple harmonic motion, derived on this page. The 0.0511 and 0.00201 constants follow from them: (2π)² / (2 × 386.09) and (2π)² / (2 × 9806.65).