The Department of Aeronautical and AutomobilecoretheorySem 3
AIRCRAFT DESIGN
AAE 3221
Syllabus
- 01Overview of the Design Process
- 02Airfoil and Geometry Selection
- 03Design constraint diagram - Thrust-to-Weight Ratio and Wing Loading
- 04Takeoff Weight and Empty weight
- 05Initial Sizing
- 06Control-Surface Sizing
- 07Engine selection
- 08Configuration Layout - Wing, Landing Gear and Engine location
- 093 View diagram
- 10Aerodynamic Considerations
- 11Structural Considerations
- 12Vulnerability Considerations
- 13Propulsion and Fuel System Integration
- 14Design Cycle of a New Design – Feasibility
- 15Configuration Design
- 16Detailed Design phases - Aerodynamics
- 17Propulsion
- 18Flight Performance
- 19Structures and Loads
- 20Weight and CG
- 21Group Weights Method
- 22Longitudinal Static Stability and Control
- 23Lateral-Directional Static Stability and Control and Handling Qualities
- 24Design Compliance Matrix
References
- Leland Nicolai, Grant Carichner, Fundamentals of aircraft and airship design, AIAA Educational Series (2010)
- Daniel P Raymer, Aircraft Design – A Conceptual approach, AIAA series (2018)
- Lloyd R Jenkinson, Paul Simpkin, Parren Rhodes ,Civil Jet Aircraft Design , AIAA series()
- L. R Jenkionson, J.F. Machman, Aircraft Design projects for engineering students ,Butterworth Heinemann (2003)
- Steven A. Brandt , Randall J. Stiles, John J. Bertin, Ray Whitford ,Introduction to Aeronautics: A Design Perspective, AIAA Education Series (2015)
Credits Structure
3Lecture
1Tutorial
0Practical
4Total