DERSLER

Şimdiye kadar verilen dersler:

Uçak Statiği, İleri Uçak Mukavemeti (Y. Lisans), Aeroelastik Olaylar (Y. Lisans), Makina ve Uçak Bilgisi, Mukavemet, Computer Programming (Y. Lisans), Dinamik, Uçak Mukavemeti, Statik, İleri Mukavemet, Uçak İnşaatı, Helikopter Aerodinamiği, Hava-Uzay Yapıları I ve Hava-Uzay Yapıları II, Uçak Tasarımı, Uçak Yapıları, Optimization Techniques in Engineering (Y. Lisans), Rüzgar Enerjisi ve Dönüştürme Teknolojisi (Y.Lisans), Structural Optimization (Lisansüstü), Rotorcraft Design I, Uçak İnşaatı ve Projesi (H. H. Okulu), Uçuş Mekaniği (H. H. Okulu), Stabilite ve Kontrol (H. H. Okulu), Uçak Yapı Analizi (H. H. Okulu),

Lisans Dersleri:

2006-2007 Eğitim-Öğretim yılı Bahar dönemi

 

Uçak Tasarımı (2+2):    Yıliçi sınavı  adedi: 1       Ağırlığı: 15

                              Ödev   adedi:        3      Ağırlığı: 15

                              Proje        adedi:   1       Ağırlığı: 30

                               Yıl  sonu sınavı      1       ağırlığı:   40

   Ders Kitapları: 1) Daniel P. Raymer, “Aircraft Design: A Conceptual Approach, Fourth Edition AIAA, 2006

                               2) Daniel P. Raymer, “ RDS-STUDENT:Software for Aircraft Design, Sizing, and Performance, Enhanced and Enlarged, Version 4.2, AIAA Education Series, 1999

                                3) Lloyd R. Jenkinson ve diğ. “Civil Jet Aircraft Design”, AIAA, 1999

Y. Lisans:

Rotorcraft Design I  (2006/2007 Güz Dönemi)

 Grading:

A  Exams:

                  1)   One Exam will be given worth 40%.

2)   One Individual Project on Conceptual Design Sensitivity Analysis for particular set of requirements will be included in the course worth 30%.

3)   One Team Project on Configuration Synthesis and Selection for a particular set of requirements will be included in the course worth 30%

 Course Schedule:

Week 1:

Course Outline Presentation:Overview of V/STOL Aircraft and Where Rotorcraft Fit In, Overview of Rotorcraft Configuration Synthesis

Week 2:

Aerodynamics Review - Hovering Flight

Aerodynamics Review - Forward Flight

Week 3:

Compound Configurations -Lift & Propulsion Sharing

Wind Tunnel Testing

Week 4:

Propulsion Review -System Analysis and Engine Characteristics and Selection, Rotor and Propeller Analysis

Week 5:

Propulsion Review - Other Propulsive Devices

Rotor Hub Design - PD, HQ, Hinges&Dynamics

Week  6:

Rotor Hub Design

A/G Resonance, S&W, FD Controls, RS&D, Ideal Rotor

Week 7 :

Helicopter Preliminary Design

Parametric Analysis

Week 8:

Techniques of Configuration : The RF Method

Week 9:

Extension of the RF Method to V/STOL Aircraft to Mission Performance,  Hover Ceiling, Range/End ROC

Week 10:

MID-TERM EXAM, Introduction to Individual Design Project

Week 11:      Introduction to Rotorcraft Structural Design - Static Loads and Strength, V-n Diagram, Rotorcraft Dynamics Design Considerations – Fatigue, Loads and Life

Week 12:      Rotorcraft Stability & Control, Design Considerations – Trim and Static Stability Derivatives, Dynamic and Control Stability

Week 13: Introduction to Team Design Project, Rotorcraft Transmission/Drive System Design and Rotorcraft Aerodynamic & Noise Design Considerations

Week 14:

Rotorcraft Safety & Reliability Design and Rotorcraft Life Cycle Cost Design Considerations

Week 15:

Team Project Presentations and Team Final Reports Due

 

Textbook and Class Materials

A.   Primary Text (PT):

Chapter 3, Engineering Design Handbook: Helicopter Engineering, Part One – Preliminary Design, AMC Pamphlet 706-201, HQS, U.S. Army Materiel Command, Aug 74 (Will be handed out in class)

 

B. Secondary Text (ST):

Leishman, J.G., Principles of Helicopter Aerodynamics, 2000, Cambridge

University Press

 

C. Thirdry Text (TT)

Hanson, T.F. A Designer Friendly Handbook of Helicopter Rotor Hubs, November,

1998, Revised November, 2001 (Will be handed out in class)

 

D.   Course Notes (CN):

Additional Course Notes (CN) will be given out in class (or made available on Dr. Tolun’s Web site) to complement the text materials. www.uubf.itu.edu.tr/~tolun

 

Wind Energy and Converting Technologies

n       Textbook and Class Materials

 

Primary Texts (PT):

        (1)T. Burton et.al.,Wind Energy, Wiley , 2001

        (2)  J.F. Manwell, J.G.McGowan, A.L. Rogers, Wind Energy Explained, John Wiley& Sons, 2002

Secondary Text (ST):

                David A. Spera, Ed., Wind Turbine Technology – Fundamental Concepts of Wind Turbine Engineering, ASME Press, 1994

Course Notes (CN):

        Additional Course Notes (CN) will be given out in class to complement the text materials

 

A.    Exams

1)     One Mid-term Exam will be given worth 20%.

2)     Final Exam and project presentation will be given worth 40%

B. Projects

1)    One Individual Project on Wind Energy Assessment for a particular site will be included in the course worth 20%.

2)   One Project on Wind Energy Converting System for a particular site will be included in the course, worth 20%

 

 Week 1    Overview of Wind Turbines,

Week 2     Wind resources, Wind Characteristics       

Week 3     Aerodynamics of WT

Week 4     Safety and Reliability of WT

Week 5     Mechanics and Dynamics

Week 6     Electrical Aspects of WT

Week 7     Wind Turbine Design

Week 8     Mid-term Exam and WT Control

Week 9     WT Siting, System Design and Integration

Week 10   Structural Dynamic Considerations in Design

Week 11    Utility Perspective on WT

Week 12   WT Acoustics and Fatigue Design of WT

Week 13   Wind Energy System Economics

Week 14   Environmental Aspects and Impacts and Project presentations

                Final reports