Araştırma Makalesi

Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils

Cilt: 28 Sayı: 3 23 Aralık 2024
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Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils

Öz

This study aims to define new simple shape descriptors to analyze airfoils. The ImageJ platform is used to calculate twelve different shape descriptors such as area, convex hull, contour temperature and solidity by performing image processing. One of the most important findings is that an increase in the thickness of an airfoil leads to corresponding increases in its area, perimeter, area of minimum enclosing area, and convex hull area. Another noteworthy discovery is that the values derived from these basic features, either increasing or decreasing. Simple shape features in the study are not used independently, as they do not possess distinct characteristics that set them apart from one another. Machine learning and deep learning applications can achieve greater success when these features are combined with other elements. The combination of these features with other shape attributes, such as chain code histograms, shape signatures, and central moments, can enhance the success of machine learning and deep learning applications.

Anahtar Kelimeler

Kaynakça

  1. [1] Santos, M., Mattos, B., Girardi, R. 2008. Aerodynamic coefficient prediction of airfoils using neural networks. 46th AIAA aerospace sciences meeting and exhibit. P.887.
  2. [2] Du, X., He, P., Martins, J.R. 2021. Rapid airfoil design optimization via neural networks-based parameterization and surrogate modeling. Aerospace Science and Technology 113.106701.
  3. [3] Chen, H., He, L., Qian W., Wang, S. 2020. Multiple aerodynamic coefficient prediction of airfoils using a convolutional neural network. Symmetry. 12(4) 544.
  4. [4] Raymer, D. 2012. Aircraft design: a conceptual approach. American instute of aeronautics and astronautics.
  5. [5] Birajdar, M.R., Kale, S.A. 2015. Effect of leading edge radius and blending distance from leading edge on the aerodynamic performance of small wind türbine blade airfoils. International journal of energy and power engineering. 4 (5-1)54-58.
  6. [6] Lim, J.W. 2018. Application of parametric airfoil design for rotor performance improvement. https://dspaceerf.nlr.nl/server/api/core/bitstreams/d428da1f-ca7a-4baf-93090924a609721e/content (Erişim Tarihi: 14.10.2024).
  7. [7] Santos, M., Mattos, B., & Girardi, R. 2008, January. Aerodynamic coefficient prediction of airfoils using neural networks. In 46th AIAA aerospace sciences meeting and exhibit (p. 887).
  8. [8] Zhang, Y., Sung, W. J., & Mavris, D. N. 2018. Application of convolutional neural network to predict airfoil lift coefficient. In 2018 AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference (p. 1903).

Ayrıntılar

Birincil Dil

İngilizce

Konular

Sinyal İşleme

Bölüm

Araştırma Makalesi

Yayımlanma Tarihi

23 Aralık 2024

Gönderilme Tarihi

19 Ekim 2024

Kabul Tarihi

14 Aralık 2024

Yayımlandığı Sayı

Yıl 2024 Cilt: 28 Sayı: 3

Kaynak Göster

APA
Tuna, H., & Yırtıcı, Ö. (2024). Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils. Süleyman Demirel Üniversitesi Fen Bilimleri Enstitüsü Dergisi, 28(3), 570-579. https://doi.org/10.19113/sdufenbed.1570399
AMA
1.Tuna H, Yırtıcı Ö. Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils. Süleyman Demirel Üniv. Fen Bilim. Enst. Derg. 2024;28(3):570-579. doi:10.19113/sdufenbed.1570399
Chicago
Tuna, Haydar, ve Özcan Yırtıcı. 2024. “Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils”. Süleyman Demirel Üniversitesi Fen Bilimleri Enstitüsü Dergisi 28 (3): 570-79. https://doi.org/10.19113/sdufenbed.1570399.
EndNote
Tuna H, Yırtıcı Ö (01 Aralık 2024) Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils. Süleyman Demirel Üniversitesi Fen Bilimleri Enstitüsü Dergisi 28 3 570–579.
IEEE
[1]H. Tuna ve Ö. Yırtıcı, “Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils”, Süleyman Demirel Üniv. Fen Bilim. Enst. Derg., c. 28, sy 3, ss. 570–579, Ara. 2024, doi: 10.19113/sdufenbed.1570399.
ISNAD
Tuna, Haydar - Yırtıcı, Özcan. “Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils”. Süleyman Demirel Üniversitesi Fen Bilimleri Enstitüsü Dergisi 28/3 (01 Aralık 2024): 570-579. https://doi.org/10.19113/sdufenbed.1570399.
JAMA
1.Tuna H, Yırtıcı Ö. Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils. Süleyman Demirel Üniv. Fen Bilim. Enst. Derg. 2024;28:570–579.
MLA
Tuna, Haydar, ve Özcan Yırtıcı. “Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils”. Süleyman Demirel Üniversitesi Fen Bilimleri Enstitüsü Dergisi, c. 28, sy 3, Aralık 2024, ss. 570-9, doi:10.19113/sdufenbed.1570399.
Vancouver
1.Haydar Tuna, Özcan Yırtıcı. Investigation of Simple Shape Descriptors for NACA 4 Digit Airfoils. Süleyman Demirel Üniv. Fen Bilim. Enst. Derg. 01 Aralık 2024;28(3):570-9. doi:10.19113/sdufenbed.1570399

e-ISSN :1308-6529
Linking ISSN (ISSN-L): 1300-7688

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