USTH SVNCKH 2026Consolation Prize

Reading cracks through vibration

A student research portfolio combining ANSYS modal analysis with Random Forest models to diagnose faults in aircraft engine fan blades.

ResearchersBùi Nhật Minh · Nguyễn Hoàng Minh
SupervisorDr. Bùi Quang Thành
InstitutionUSTH, Hanoi
Blue three-dimensional fan blade with modal contour waves and a crack marker
Signal0.131%median shift
Dataset55,350readings
Modes01-10frequency features
515valid crack geometries
90readings per blade case
5-foldgrouped cross-validation
2.88 mfull-scale blade
01
Research question

From a subtle signal
to a useful diagnosis.

Can changes in a blade’s first ten natural frequencies distinguish a healthy blade from a cracked one-and support localisation and sizing?

The challenge is scale: on a full-size blade, many crack signatures are comparable to realistic measurement noise.

Q11

Represent

Model crack position, length, and depth correctly on a curved, twisted blade.

Q22

Quantify

Measure how each crack geometry changes the first ten natural frequencies.

Q33

Detect

Find which cracks remain distinguishable after measurement uncertainty is introduced.

02
Method · Connected pipeline

Physics in.
Evidence out.

Every stage feeds the next, while the physical blade case remains the independent sample throughout evaluation.

01CAD

Blade model

CATIA geometry, Ti-6Al-4V material, and a fully clamped root.

02FEA

Mesh verification

654,966 SOLID187 elements; convergence checked at three densities and against APDL.

03Physics

Crack representation

Local stiffness reduction with depth measured along the curved surface normal.

04Dataset

Case generation

600 Latin Hypercube samples spanning position, length, and depth; 515 valid cracks.

05Signal

Noise modelling

Three Gaussian relative-noise levels and repeated readings for realistic evaluation.

06ML

Grouped evaluation

Case-grouped split and five-fold grouped cross-validation prevent reading-level leakage.

CATIA V5ANSYS 2024 R1PyMAPDLPythonscikit-learn
03
Results · Operating boundary

Detection works.
Sizing does not-yet.

Repeated low-noise measurements improve classification, while frequency-only features remain too weak for precise crack sizing.

Crack recall93.2%

Case-level recall at the calibrated safety-first threshold.

Healthy specificity80.0%

Trade-off retained while prioritising missed-crack risk.

Geometry prediction R²0.04-0.14

The report explicitly rejects deployment for reliable sizing.

Balanced accuracy by noise level

Averaging helps most when the signal is clean.

At 0.1% simulated noise, prediction averaging increases balanced accuracy from 60.4% to 87.6%. The advantage narrows quickly as noise rises.

Single readingPrediction average
050100%
0.1%noise
60.4
87.6
0.5%noise
52.0
61.7
1.0%noise
50.3
53.8
04
Evidence & limitations

The blade case-not the reading-is the sample.

Correlated readings never cross splits. That design decision makes the reported performance substantially more credible.

Train492physical cases
Validation5 foldsgrouped CV
Held out123physical cases
LeakageZerocase overlap
01

Numerical evidence

Simulation-based results have not yet been validated on a physical fan blade.

02

Healthy diversity

Healthy cases are noisy realisations of one baseline, not independent blade geometries.

03

Model scope

The clamped blade at rest omits rotational prestress, coupling, mistuning, and crack breathing.

04

Evaluation caveat

A future untouched simulation batch is needed for a strictly unbiased estimate.

05
Academic recognition

Consolation Prize
USTH SVNCKH 2026

The project received one of two Consolation Prizes in its evaluation panel. The university-wide competition featured 27 projects evaluated across three panels.

This states the official award category without implying an overall fourth-place ranking.
USTH2026Student research
06
Research artifacts

Inspect the complete evidence.

The 20-page report records the assumptions, dataset, grouped evaluation and limitations. The A0 poster presents the competition-ready summary.

A0 poster summarising the fan-blade fault-diagnosis researchOpen A0 poster
07
Selected references

Grounded in structural health monitoring and supervised learning.

  1. Yang et al. - Engineering Failure Analysis, 2025
  2. Henderson et al. - Sensors, 2024
  3. Gillich et al. - Sensors, 2022
  4. Breiman - Random Forests, Machine Learning, 2001
  5. Pedregosa et al. - Scikit-learn, JMLR, 2011