Havacılık ve Uzay Mühendisliği

AE 306 | Ders Tanıtım Bilgileri

Dersin Adı

High Speed Aerodynamics

Kodu	Yarıyıl	Teori (saat/hafta)	Uygulama/Lab (saat/hafta)	Yerel Kredi	AKTS
AE 306	FALL	3	0	3	6

Ön-Koşul(lar)	AE 301 to succeed (To get a grade of at least DD)
Dersin Dili	English
Dersin Türü	ELECTIVE_COURSE
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)	-

Dersin Amacı

This course aims to explain the basic principles of high-speed aerodynamics, to teach compressible flow, normal and oblique shock waves, supersonic and supersonic flows, and to strengthen the knowledge base through weekly assignments.

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 compressibility effects in aerodynamics,				X
LO2	Define normal shock waves,				X
LO3	Identfy oblique shock waves,					X
LO4	Determine compressible flow through nozzles, diffusers				X
LO5	Model flow based on linear theory,			X

Ders Tanımı

The High Speed Aerodynamics course covers important issues in understanding the aerodynamic design process, and in this context, it particularly covers the modeling of compressible flow and some calculation methods.

Dersin İlişkili Olduğu Sürdürülebilir Kalkınma Amaçları

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

HAFTALIK KONULAR VE İLGİLİ ÖN HAZIRLIK ÇALIŞMALARI

Hafta	Konular	Ön Hazırlık	Öğrenme Çıktısı
1	Compressible flow: some basics, brief review of thermodynamics, governing equations of compressible flow.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 7.	LO1
2	Compressible flow: some basics, brief review of thermodynamics, governing equations of compressible flow.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 7.	LO1
3	Normal shock waves, normal shock wave equations.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 8.	LO2
4	Normal shock waves, normal shock wave equations.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 8.	LO2
5	Oblique shock and expansion waves, oblique shock relations, shock wave interference and reflections, Prandtl-Meyer expansion waves, shock wave expansion theory.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 9.	LO3
6	Oblique shock and expansion waves, oblique shock relations, shock wave interference and reflections, Prandtl-Meyer expansion waves, shock wave expansion theory.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 9.	LO3
7	Oblique shock and expansion waves, oblique shock relations, shock wave interference and reflections, Prandtl-Meyer expansion waves, shock wave expansion theory.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 9.	LO3
8	Midterm		-
9	Compressible flow in nozzles, diffusers and wind tunnels, governing equations of quasi-one dimensional flow, nozzle flow, supersonic wind tunnels.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 10.	LO4
10	Compressible flow in nozzles, diffusers and wind tunnels, governing equations of quasi-one dimensional flow, nozzle flow, supersonic wind tunnels.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 10.	LO4
11	Compressible flow in nozzles, diffusers and wind tunnels, governing equations of quasi-one dimensional flow, nozzle flow, supersonic wind tunnels.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 10.	LO4
12	Subsonic compressible flow around an airfoil, linearity theory, linear velocity potential theory.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 11.	LO5
13	Subsonic compressible flow around an airfoil, linearity theory, linear velocity potential theory.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 11.	LO5
14	Prandtl-Glauert compressibility correction, Mach number, sound barrier, area rule and supercritical airfoils.	Fundamentals of Aerodynamics. J. D. Anderson, Jr., McGraw Hill Series in Aeronautical and Aerospace Engineering, McGraw-Hill, ISBN 0-07-237335-0, Ch. 11.	LO5
15	Semester Review		-
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
Ödev	5	25	X	X	X	X	X
Ara Sınav	1	25	X	X	X
Final Sınavı	1	50	X	X	X	X	X
Toplam	7	100

AKTS / İŞ YÜKÜ TABLOSU

Yarıyıl Aktiviteleri	Sayı	Süre (Saat)	İş Yükü
Katılım	-	-	-
Teorik Ders Saati	16	3	48
Laboratuvar / Uygulama Ders Saati	-	-	-
Sınıf Dışı Ders Çalışması	14	6	84
Arazi Çalışması	-	-	-
Küçük Sınav / Stüdyo Kritiği	-	-	-
Portfolyo	-	-	-
Ödev	5	5	25
Sunum / Jüri Önünde Sunum	-	-	-
Proje	-	-	-
Seminer/Çalıştay	-	-	-
Sözlü Sınav	-	-	-
Ara Sınavlar	1	10	10
Final Sınavı	1	13	13
		Toplam	180