Havacılık ve Uzay Mühendisliği

AE 304 | Ders Tanıtım Bilgileri

Dersin Adı

Flight Mechanics

Kodu	Yarıyıl	Teori (saat/hafta)	Uygulama/Lab (saat/hafta)	Yerel Kredi	AKTS
AE 304		3	0	3	5

Ön-Koşul(lar)	AE 301 to succeed (To get a grade of at least DD)
Dersin Dili	English
Dersin Türü	-
Dersin Düzeyi	-
Dersin Veriliş Şekli	Face to Face
Dersin Öğretim Yöntem ve Teknikleri	-
Ulusal Meslek Sınıflandırma Kodu	-
Dersin Koordinatörü	-
Öğretim Eleman(lar)ı	-
Yardımcı(ları)	-

Dersin Amacı

The purpose of this course is to examine the motion of aircraft in the atmosphere and predict their performance.

Öğrenme Çıktıları

Bu dersi başarıyla tamamlayabilen öğrenciler;

Ad	Açıklama	PC Alt	* Katkı Düzeyi
Ad	Açıklama	PC Alt	1	2	3	4	5
LO1	Describe aerodynamics of a whole aircraft.				X
LO2	Compare different aircraft propulsion systems.					X
LO3	Solve equations of motion in three dimensional environments.				X
LO4	Solve equations related to steady flight; equations of motion for steady, level flight.					X
LO5	Calculate the take-off and the climb performance of an aircraft.				X
LO6	Determine the cruise, descending, and landing performance of aircraft.			X
LO7	Design aerodynamics test.				X

Ders Tanımı

Flight Mechanics course provides important information about understanding the motion of the aircraft. In this context, firstly trajectory analysis, then performance issues, and also calculations related to the mentioned issues are discussed.

Dersin İlişkili Olduğu Sürdürülebilir Kalkınma Amaçları

Dersin Kategorisi	Temel Ders
	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	Evaluation of Aircraft and Their Performance, Brief History	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 1.	LO1
2	Aircraft Aerodynamics: Drag Poles; Source of Aerodynamic Forces, Aerodynamic Coefficients, Aerodynamic Center.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 2	LO1
3	Aircraft Aerodynamics: Drag Poles; NACA Profile Definitions, Lift and Drag Configuration, Drag Poles, Historical Note: The Birth of Drag Poles.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 2	LO1
4	Some Propulsion System Characteristics; Thrust and Efficiency, Propeller Engines, Turbojet Engine.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 3	LO2
5	Some Propulsion System Characteristics; Evaluations on Turbofan Engine, Turboprop Engine, Afterburner Systems and Fuel Consumption.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 3	LO2
6	Equations of Motion.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 4	LO3
7	Aircraft Performance: Steady Flight; Equations of Motion for Steady Flight, Level Flight, Thrust Requirement (Drag), Fundamental Parameters, Thrust-to-Weight Ratio, Wing Loading, Drag Polar, Lift-to-Drag Ratio, Aircraft Maximum Speed and Thrust.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 5	LO4
8	Midterm		-
9	Aircraft Performance: Steady Flight; Power Requirement, Top Speed and Power, Effect of Divergent Drag Increase on Top Speed, Minimum Speed, Total Separation and Lift Augmentation Systems.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 5	LO4
10	Aircraft Performance: Sustained Flight; Rate of Climb, Service and Absolute Ceiling, Time to Climb.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 5	LO5
11	Aircraft Performance: Sustained Flight; Range, Endurance, Overall Evaluations of Range and Endurance.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 6	LO4
12	Aircraft Performance: Accelerated Flight; Level Turn, Nose-Up and Nose-Down Maneuvers.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 6	LO4
13	Aircraft Performance: Accelerating Flight; Constraint Case at High Load Factors, V-n Diagram.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 6	LO4
14	Aircraft Performance: Accelerated Flight; Energy Approaches, Accelerated Rate of Climb, Takeoff Performance, Landing Performance.	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 6	LO6
15	Review	Aircraft Performance and Design, John D. Anderson, Mc-Graw-Hill Company, Ch. 6	-
16	Final		-

Ders Kitabı	Aircraft Performance and Design John D. Anderson Mc-Graw-Hill Company ISBN-13:978-0-07-070245-5.
Önerilen Okumalar/Materyaller	Airplane Design Jan Roskam Part VII: Determination of stability control and performance characteristics Roskam Aviation and Engineering Corporation.

DEĞERLENDİRME ÖLÇÜTLERİ

Yarıyıl Aktiviteleri	Sayı	Katkı Payı %	LO1	LO2	LO3	LO4	LO5	LO6	LO7
Ödev	5	15		X	X	X	X	X
Proje	1	10							X
Ara Sınav	1	25	X	X	X	X
Final Sınavı	1	50	X	X	X	X	X	X	X
Toplam	8	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	3	42
Arazi Çalışması	-	-	-
Küçük Sınav / Stüdyo Kritiği	-	-	-
Portfolyo	-	-	-
Ödev	5	4	20
Sunum / Jüri Önünde Sunum	-	-	-
Proje	-	-	-
Seminer/Çalıştay	-	-	-
Sözlü Sınav	-	-	-
Ara Sınavlar	1	20	20
Final Sınavı	1	20	20
		Toplam	150