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Data Driven Benchmark - Plate with Hole - Dataset 4

Inspired by strategic discussions within the NAFEMS ASSESS Initiative, this curated finite element analysis dataset builds upon NAFEMS' 40-year legacy of establishing trusted industry benchmarks for physics-based simulation and looks to the emerging use of AI in engineering simulation.

The collection provides baseline data on principal stress distributions within plate geometries. A deliberately simple problem was selected to maximise the dataset's educational merit. Because the peak principal stress for this geometry can be validated against a well-established analytical solution (Heywood's equations), the dataset provides a transparent baseline. This simplicity allows engineers and researchers to study fundamental behaviour of the data driven models, such as demonstrating how the quantity and distribution of training data impacts the model predictions. As artificial intelligence models increasingly integrate into commercial simulation tools, this dataset is intended to serve as a useful resource for engineers looking for a vendor neutral dataset.

To maintain NAFEMS' commitment to vendor neutrality, the results are provided in the open standard VMAP format, alongside training and test data in HyperMesh (*.h3d) and Nastran (*.op2) formats. For those who wish to recreate the results on their own systems solver input decks have been provided in optistruct (*.fem) and Nastran (*.bdf) format.

Download the problem description

NAFEMS would like to thank Altair and the Fraunhofer Institute for their support with this project.

P​roblem Variables

V​ariable

Range Lower Bound

R​ange Upper Bound

H​ole diameter

30mm

2​40mm

P​late width

300mm

1​000mm

P​late length

3​00mm

1​000mm

P​late thickness

1​mm

2​0mm

A​pplied load

5​000N

1​00000N

O​ffset width direction

0​mm

0​.4 x (Plate Width - Hole diameter)

O​ffset length direction

0​mm

0​.4 x (Plate Length - Hole diameter)

T​he Datasets

6​ datasets have been provided. The first 5 datasets are relatively simple and vary between one and three parameters.

The 6th dataset represents a significantly more complicated problem where 7 parameters are varied. T​he variables in the 6th dataset have been selected using latin hypercube sampling approach. Users are encouraged to parse the dataset for outliers.

Dataset

# training sets

# test sets

Variables

Dataset location

1

19

3

H​ole diameter

Link

2

19

6

Hole diameter, p​late thickness

L​ink

3​

1​9

3​

H​ole Diameter, plate width, plate length

L​ink

4​

1​9

3​

H​ole diameter, applied load

N​AFEMS Member Download Button

5​

1​9

3​

H​ole diameter, hole location

L​ink

6​

9​7

-​

H​ole diameter, plate thickness, applied load, plate width, plate length, hole location

L​ink

Dataset 4 Details

I​D

T​est/ Train

Diameter (mm)

T​hickness (mm)

W​idth (mm)

L​ength (mm)

WidthOffset (mm)

LengthOffset (mm)

Load (N)

Test41

Test

45

5

300

600

0

0

7000

Test42

Test

140

5

300

600

0

0

50000

Test43

Test

200

5

300

600

0

0

75000

Train 41

Train

30

5

300

600

0

0

47500

Train 42

Train

53

5

300

600

0

0

68500

Train 43

Train

77

5

300

600

0

0

78900

Train 44

Train

100

5

300

600

0

0

73700

Train 45

Train

123

5

300

600

0

0

100000

Train 46

Train

147

5

300

600

0

0

36800

Train 47

Train

170

5

300

600

0

0

84200

Train 48

Train

193

5

300

600

0

0

10500

Train 49

Train

217

5

300

600

0

0

57900

Train 410

Train

240

5

300

600

0

0

15800

Train 411

Train

30

5

300

600

0

0

5300

Train 412

Train

53

5

300

600

0

0

26300

Train 413

Train

77

5

300

600

0

0

89500

Train 414

Train

100

5

300

600

0

0

42100

Train 415

Train

123

5

300

600

0

0

52600

Train 416

Train

147

5

300

600

0

0

21100

Train 417

Train

170

5

300

600

0

0

63200

Train 418

Train

193

5

300

600

0

0

31600

Train 419

Train

217

5

300

600

0

0

94700

 

Document Details

Referenceassess-26-04
AuthorSymington. I
LanguageEnglish
AudiencesAnalyst Developer
TypeKnowledge Base
Date 22nd February 2026
OrganisationNAFEMS

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