ANK307/308 Aircraft Design

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ANK307 Aircraft Design 1

Analyses of: trends, costs, mission, weight, thrust and wing loading. Fuselage and ergonomics. Wings and empennages. High lift devices and control surfaces. Landing gear. Propulsion integration. Loads and handling qualities.

ANK308 Aircraft Design 2

Loads and handling qualities. Types of structures applicable in aircraft design. Wing and empennages components and their structures. Fuselage components and their structures. Simplified methods of strength calculations. Connections between fuselage, wing and empennages. Mechanical control systems.

Announcement:

News:

Aircraft Design 1

ank307_1

Rules of crediting and deadlines

Projects:

  1. Initial analyses
  2. Feasibility study
  3. Initial design and detailed weight analysis
  4. Aerodynamic characteristics
  5. Flight envelope and loads envelope

Lecture handouts:

  1. Introductory lecture
  2. Wing and thrust loading selection and cost analysis
  3. Fuselage
  4. Landing gear
  5. Propulsion
  6. Empennages
  7. Airplane drawing
  8. Wings
  9. High lift devices and control surfaces
  10. Dynamic stability
  11. Handling qualities (longitudinal & lateral)
  12. Loads envelope and loads of the wing
  13. Loads of the horizontal tail
  14. Loads of the fuselage
  15. Loads of landing gear and control system

Marks:

     Example of the 2nd colloquium problem

Aircraft Design 2

ank307_2

Rules of crediting and deadlines

Projects:

  1. Longitudinal static stability and lateral control
  2. Wing loads
  3. Aeroplane structure
  4. Fuselage loads
  5. Fitting design

Lecture handouts:

  1. Introductory lecture
  2. Wing structure and simplified spar analysis
  3. Simplified wing-box analysis
  4. Skins, ribs and longerons
  5. Fuselage and fuselage-wing connection
  6. Empanages
  7. Control surfaces and high lift devices structures
  8. Stabilizers installation

Colloquium useful links:

Marks

Colloquium

Colloquium - improvement

Colloquium - improvement 2

Colloquium - the last improvement