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AE 301 | Ders Tanıtım Bilgileri

Dersin Adı

Aerodynamics

Kodu	Yarıyıl	Teori (saat/hafta)	Uygulama/Lab (saat/hafta)	Yerel Kredi	AKTS
AE 301	FALL	2	2	3	5

Ön-Koşul(lar)	None
Dersin Dili	English
Dersin Türü	Zorunlu
Dersin Düzeyi	Lisans
Dersin Veriliş Şekli	Face to Face
Dersin Öğretim Yöntem ve Teknikleri	-
Ulusal Meslek Sınıflandırma Kodu	-
Dersin Koordinatörü	Dr. Öğr. Üyesi İzzet Murat Akşit
Öğretim Eleman(lar)ı	Dr. Öğr. Üyesi İzzet Murat Akşit
Yardımcı(ları)	Araş. Gör. Hasan Totoş

Dersin Amacı

This course aims to present the basic principles of low speed aerodynamics including inviscid and incompressible flow, to provide common methods used in aerodynamic design stages, and to intensify the knowledge by means of weakly homeworks.

Öğrenme Çıktıları

Bu dersi başarıyla tamamlayabilen öğrenciler;

Ad	Açıklama	PC Alt	* Katkı Düzeyi
Ad	Açıklama	PC Alt	1	2	3	4	5
LO1	Describe the importance of aerodynamics.			X
LO2	Define fundamental knowledge of aerodynamic forces and moments, aerodynamic coefficients.					X
LO3	Model the flow based on conservation laws.				X
LO4	Describe the generation of lift.				X
LO5	Compare the aerodynamic shapes including cylinder and airfoil,				X
LO6	Discuss lifting surface theory and wing. (Aerodynamic test using wind tunnel.)					X

Ders Tanımı

Aerodynamics course provides important tools in understanding of aerodynamic design process. The course is composed of the topics related to mainly inviscid and incompressible flow modeling and computations.

Dersin İlişkili Olduğu Sürdürülebilir Kalkınma Amaçları

Dersin Kategorisi	Temel Ders	X
	Uzmanlık/Alan Dersleri
	Destek Dersleri
	İletişim ve Yönetim Becerileri Dersleri
	Aktarılabilir Beceri Dersleri

HAFTALIK KONULAR VE İLGİLİ ÖN HAZIRLIK ÇALIŞMALARI

Hafta	Konular	Ön Hazırlık	Öğrenme Çıktısı
1	Aerodynamics: some introductory thoughts; aerodynamic forces and moments, coefficients, dimensional analysis and the Buckingham Pi theorem.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 1.	LO1
2	Aerodynamics: some introductory thoughts; flow similarity, types of flows.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 1.	LO1
3	Aerodynamics: some fundamental principles and equations; review of vector relations, integrals, models of the fluid, control volumes and fluid elements	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 2.	LO2
4	Aerodynamics: some fundamental principles and equations; conservation laws including continuity equation, momentum equation, and energy equation.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 2.	LO2
5	Aerodynamics: some fundamental principles and equations; flow patterns, vorticity, circulation, velocity potential and stream function, some introductory information about numerical solutions based on computational fluid dynamics.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 2.	LO3
6	Fundamentals of inviscid, incompressible flow: Bernoulli’s equation, incompressible flow in a duct, pitot tube, pressure coefficient	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 3.	LO3
7	Fundamentals of inviscid, incompressible flow: governing equations for irrotational, incompressible flow, Laplace’s equation, uniform flow, source flow.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 3.	LO3
8	Midterm		-
9	Fundamentals of inviscid, incompressible flow: doublet flow, vortex flow, the Kutta-Joukowski theorem and generation of lift, panel methods	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 4.	LO3
10	Incompressible flows over airfoils: airfoil nomenclature and characteristics, the vortex sheet, the Kutta condition, Kelvin’s circulation theorem. /Experiment	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 4.	LO3
11	Incompressible flows over airfoils: classical thin airfoil theory, the aerodynamic center, modern low speed airfoils./Experiment	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 4.	LO4
12	Incompressible flow over finite wings: Prandtl’s classical lifting line theory, a numerical nonlinear lifting line method, lifting surface theory and vortex lattice numerical method. /Experiment	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 5.	LO4
13	Incompressible flow over finite wings: Prandtl’s classical lifting line theory, a numerical nonlinear lifting line method, lifting surface theory and vortex lattice numerical method./Experiment	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 5.	LO5
14	Carrier line theory, elliptical carrier distribution./Experiment	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 6.	LO6
15	Review /Experiment		-
16	Final		-

Ders Kitabı	Fundamentals of Aerodynamics. J. D. Anderson Jr. McGraw Hill Series in Aeronautical and Aerospace Engineering McGraw-Hill ISBN 0-07-237335-0.
Önerilen Okumalar/Materyaller	Aerodynamics for Engineering Students E. L. Houghton and P. W. Carpenter Butterworth Heinemann ISBN 0 7506 5111 3

DEĞERLENDİRME ÖLÇÜTLERİ

Yarıyıl Aktiviteleri	Sayı	Katkı Payı %	LO1	LO2	LO3	LO4	LO5	LO6
Laboratuvar / Uygulama	5	10			X	X		X
Ödev	5	15		X	X		X
Ara Sınav	1	25	X	X	X
Final Sınavı	1	50	X	X	X	X	X	X
Ara Sınav	1	0
Toplam	13	100

AKTS / İŞ YÜKÜ TABLOSU

Yarıyıl Aktiviteleri	Sayı	Süre (Saat)	İş Yükü
Katılım	-	-	-
Teorik Ders Saati	16	2	32
Laboratuvar / Uygulama Ders Saati	16	2	32
Sınıf Dışı Ders Çalışması	14	4	56
Arazi Çalışması	-	-	-
Küçük Sınav / Stüdyo Kritiği	-	-	-
Portfolyo	-	-	-
Ödev	5	2	10
Sunum / Jüri Önünde Sunum	-	-	-
Proje	-	-	-
Seminer/Çalıştay	-	-	-
Sözlü Sınav	-	-	-
Ara Sınavlar	1	10	10
Final Sınavı	1	10	10
		Toplam	150

DERSİN ÖĞRENME ÇIKTILARININ PROGRAM YETERLİLİKLERİ İLE İLİŞKİSİ

#	PC Alt	Program Yeterlilikleri / Çıktıları	* Katkı Düzeyi
			1	2	3	4	5
Program yeterlilik verisi bulunamadı.

*1 Lowest, 2 Low, 3 Average, 4 High, 5 Highest

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