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Crack Propagation Tests for Load Sequences Developed Using Different Flight Parameters of a Trainer Aircraft Cover

Crack Propagation Tests for Load Sequences Developed Using Different Flight Parameters of a Trainer Aircraft

Open Access
|Oct 2024

Figures & Tables

Figure 1.

Location of strain gauges during the OLM and the SLM14 sensor
Location of strain gauges during the OLM and the SLM14 sensor

Figure 2.

Technical drawing of the CT samples used in the test and the mount
Technical drawing of the CT samples used in the test and the mount

Figure 3.

Test specimen mounted in the test stand, shown during (with a COD gauge) and after the test.
Test specimen mounted in the test stand, shown during (with a COD gauge) and after the test.

Figure 4.

Crack propagation curves obtained for different load spectra
Crack propagation curves obtained for different load spectra

Linear regression model parameters for the SLMX14 equations using flight parameters

Independent variablesRR2free coefficientabc
nz0.93200.8686-64.1018388.8242--
nz, Hb0.94590.8947-113.747368.2960.046-
nz, Hb, Vp0.97420.9491-231.156332.5240.0320.726

Correlation matrix for the available flight parameters

VariableSLMX14nzHbVPdhdkldldv
SLMX141.000.930.430.610.37-0.30-0.03-0.07
nz0.931.000.290.390.28-0.14-0.08-0.03
Hb0.430.291.000.300.42-0.490.090.17
VP0.610.390.301.000.22-0.46-0.08-0.15
dh0.370.280.420.221.000.08-0.040.22
dkl-0.30-0.14-0.49-0.460.081.00-0.000.15
dl-0.03-0.080.09-0.08-0.04-0.001.00-0.15
dv-0.07-0.030.17-0.150.220.15-0.151.00

Load sequence characteristics

SequenceSLMX14nznz+Hbnz+Hb + Vp
Number of cycles52894304342824125348
SFH270.6266.7267.7271

Dimensions of the CT specimens used in the test

W [mm]B [mm]Width [mm]Height [mm]Holes [fi_mm]Notch [mm]CS [mm2]Precrack [mm]H [mm]
4886057.61221.6307.213
DOI: https://doi.org/10.2478/fas-2023-0010 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
Language: English
Page range: 155 - 165
Published on: Oct 28, 2024
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year

© 2024 Piotr Reymer, Kamil Kowalczyk, Marta Baran, Dominik Nowakowski, Michał Dziendzikowski, Andrzej Leski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.