Termal Yüklere Maruz Kalan Naca 0012 Kanat Yapisinin İncelenmesi

Date

2016-10-14

Author

Özkökdemir, Emir
Acar, B
Kurtuluş, Dilek Funda

Metadata

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Süpersonik rejimde uçan kanatlar çeşitli yüklemelere maruz kalırlar. Bu yükleme tiplerinden biri olan termal yüklemeler, kanatların tasarımı üzerinde oldukça etkilidir, bu nedenle büyük öneme sahiptir. Termal yükleme kaynaklı oluşan termal gradyan kanatlar üzerinde yapısal bozulmalara yol açabilir. Bu çalışmanın amacı aerodinamik ısınma gibi termal yüklemelere maruz kalan kanatların yapısal bütünlüğü incelenmesidir. 2 boyutlu olarak yapılan karşılaştırma analizleri için literatürde bulunan NACA0012 kanat profili seçilmiştir. Hesaplamalı akışkanlar dinamiği ve sonlu elemanlar modelleri ayrı ayrı oluşturulmuş, elde edilen sonuçlar literatür verileri ile karşılaştırılmıştır.

Subject Keywords

Wing, Canard, Aerodynamic Heating, Computational Fluid Dynamics(CFD), Finite Element Methods (FEM)

URI

https://hdl.handle.net/11511/71132

Conference Name

8. Savunma Teknolojileri Kongresi , SAVTEK, 12 - 14 Ekim 2016

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

E. Özkökdemir, B. Acar, and D. F. Kurtuluş, “ Termal Yüklere Maruz Kalan Naca 0012 Kanat Yapisinin İncelenmesi,” presented at the 8. Savunma Teknolojileri Kongresi , SAVTEK, 12 - 14 Ekim 2016, Ankara, Türkiye, 2016, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/71132.