Design and analysis of an aerospace system, specifically a complete flight vehicle, aircraft or UAV, with integrated propulsion system, structural system, and control system; market analysis, operating studies, mission specifications, certification requirements; configuration selection; multidisciplinary character of design, classical design and analysis methods
Contents:
• Design process
• Flight vehicle sizing
• Geometry selection
• Thrust-to-weight ratio and wing loading
• Initial sizing
• Configuration layout and loft
• Disciplinary considerations
• Aerodynamics
• Structures
• Controls
• Propulsion and fuel system integration
• Subsystems
• Crew station, passengers, and payload
- Dozent/in: Alfred Striz