Akademik Dersler - İçerik

Explain the phases of the aircraft design process and the systems perspective of conceptual design
Translate design requirements and constraints into an aircraft configuration
Apply preliminary estimation methods for takeoff weight, empty weight, and fuel weight
Select airfoil, wing geometry, and tail arrangement based on fundamental design considerations
Determine key design parameters such as thrust-to-weight ratio and wing loading
Perform initial sizing and develop a preliminary aircraft configuration
Evaluate configuration layout in terms of aerodynamic, structural, and operational criteria
Interpret the integration of crew, payload, fuel, and propulsion systems at the conceptual design level