Astronomy & Space

TB 26-09 Measured Hammer-Tap Inputs

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Modal analysisVibration testing

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This NASA technical bulletin establishes that instrumented hammer tests for modal analysis remain valid even when the impact force deviates from an ideal half-sine waveform, including cases with ripples or separated contacts. The key requirement is accurate measurement of the complete force history and structural response, rather than achieving a perfect pulse shape. Adequacy of the test depends on measurement accuracy, bandwidth, signal-to-noise ratio, and whether the excitation covers the required frequency and amplitude ranges for the intended objective.


This guidance allows engineers to accept hammer test data that might otherwise be rejected for cosmetic deviations from ideal waveforms, reducing unnecessary test repetition and costs. It provides clear criteria for evaluating structural dynamics testing based on measurement quality and test objectives rather than arbitrary waveform appearance standards.


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For more information, contact Joel W. Sills, Langley Research Center, joel.w.sills@nasa.gov.

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An instrumented hammer test does not require an idealized single half-sine waveform. When the complete force and response are measured accurately, crest ripples and separated contacts remain known inputs. Force shape changes excitation, but does not inherently invalidate the record. Adequacy depends on measurement accuracy, bandwidth, signal-to-noise ratio, and coverage of the test objective.

Background: What the Hammer Actually Measures
Hammer tests support modal analysis [2–4] and can precede pyroshock testing [6]. Figure 1 compares a half-sine, maintained-contact rippling, and separated contacts. During a zero-force interval, the structure continues to vibrate; re-contact acts on that vibration.

If an exact model and test article receive the same force and initial conditions, uniqueness gives identical responses for each bounded measured history. An approximate model can show different errors as inputs excite different frequencies, amplitudes, or nonlinear states. See [1] for the exact-model derivation.

Analysis: A Half-Sine Is Broadband, but Not Flat
Figure 2 shows that a finite half-sine is broadband but contains spectral zeros at f/fo = 3, 5, 7, …, with fo = 1/(2T) for pulse duration T. Its appearance alone cannot establish adequate excitation.

Analysis: Spectral Content Is Determined by the Measured Force History
Figure 3 normalizes each spectrum to its own DC value. Crest rippling adds content and can fill half-sine notches. Timing between separated contacts creates deterministic interference. For adequacy, inspect the unnormalized measured spectrum and response signal-to-noise ratio.

Recommended Practice: Evaluate Test Adequacy Against the Intended Objective
• Measure the complete applied force with adequate bandwidth, calibration, dynamic range, and time synchronization.
 • Verify that the response measurements have adequate bandwidth and signal-to-noise ratio and are not clipped or saturated.
 • Confirm that the excitation covers the frequency, amplitude, and nonlinear-response ranges required by the intended test objective.
• Reject or repeat a test only for an identified measurement, excitation, or coverage deficiency.

Conclusion
Half-sine appearance neither establishes validity nor guarantees adequacy. Judge each hammer test by its purpose and by accurate, complete force and response measurements over the required range.

References
1. A. Majed, J. Sills, E. Henkel, V. Babuska, S. Yunis, D. Hamilton, J. Akers, and T. Kinney, Validity and Predictability of Measured Hammer Tap Inputs: Linear and Nonlinear Structural Systems, September 2026.
2. D. J. Ewins, Modal Testing: Theory, Practice and Application, 2nd ed., 2000.
3. ISO 7626-5:2019, Mechanical Vibration and Shock—Experimental Determination of Mechanical Mobility—Part 5
4. K. G. McConnell and P. S. Varoto, Vibration Testing: Theory and Practice, 2nd ed., 2008.
5. A. H. Nayfeh and D. T. Mook, Nonlinear Oscillations, 1979. 6. NASA-STD-7003, Pyroshock Test Criteria, 1999

Source: TB 26-09 Measured Hammer-Tap Inputs