TEXTBOOK: Aircraft Design: A Conceptual Approach OTHER ...

475 downloads 1511 Views 993KB Size Report
Stress. Weight. Wing [email protected] http://ninova.itu.edu.tr/tr/dersler/ucak-uzay- fakultesi/1005/uck-451e/. TEXTBOOK: Aircraft Design: A Conceptual Approach.
TEXTBOOK: Aircraft Design: A Conceptual Approach Raymer D. P, 2006,, Fourth Edition, AIAA Education Series, New York, NY, ISBN:1-56347-829

Fuselage

Hydrolics

Loft

Powerplant

Production

OTHER REFERENCE: Airplane Design

Aerodynamics

Armanent

Electrical

Empennage

[email protected]

Control

Equipment

Service

Wing

Stress

Weight

Roskam J., 2003,, parts: 1-8, Design, Analysis and Research (DAR) Corporation, ISBN:1-884885-42 2

http://ninova.itu.edu.tr/tr/dersler/ucak-uzay-fakultesi/1005/uck-451e/

Weeks 1 2 3 4 5 6 7 8 9 10 11 12 13 14

Topics Introduction Project Definition Competitor Study First Guess Sizing Airfoil and Geometry Selection Thrust to Weight Ratio and Wing Loading Midterm Examination Initial Sizing Configuration Layout and Loft Configuration Layout and Loft Propulsion and Fuel System Integration Landing Gear and Subsystems Aerodynamics Aerodynamics

1. Introduction to Aircraft Design Phases of aircraft design, aircraft conceptual design process, takeoff weight buildup, empty weight estimation, fuel-fraction estimation, takeoff-weight calculation

2. Airfoil and Geometry Selection Airfoil selection, wing geometry, tail geometry and arrangement

3. Thrust to Weight Ratio and Wing Loading Thrust to weight ratio, wing loading, selection of thrust to weight and wing loading

4. Initial Sizing Rubber engine sizing, fixed engine sizing, geometry sizing, control surface sizing

5. Configuration Layout and Loft End products of configuration layout, conic lofting, conic fuselage development, flat-wrap fuselage lofting, circle to square adapter, fuselage loft verification, wing tail layout and loft, aircraft layout procedures, wetted area determination, volume determination, special considerations

6. Propulsion and Fuel System Integration Propulsion selection, jet-engine performance and integration, propeller-engine performance and integration, fuel system

7. Landing Gear and Subsystems Landing gear arrangements, tire sizing, shock absorbers, castoring wheel geometry, gear retraction geometry, seaplanes, subsystems

8. Aerodynamics Aerodynamic forces, Lift, Parasite drag, Induced drag, CFD

Activities Midterm Exams

Quantity Effects on Grading, % 1

20

Projects

9

20

Term Paper/Project

1

15

1

40

Quizzes Homework

Laboratory Work Other Activities Final Exam

5