課程大綱:
本課程透過理論講述與實際設計案例進行固定翼無人機氣動力設計教學，內容包含、機翼外型與翼剖面擇優分析、全機外型設計、任務規劃與重量預估分析、及基本六自由度氣動力參數分析等，培養學生具備無人機外型設計與氣動力參數分析能力。

Course Content:
This course provides comprehensive instruction in the aerodynamic design of fixed-wing unmanned aerial vehicles (UAVs) through a combination of theoretical principles and practical aircraft design case studies. Topics include wing planform design and airfoil selection, aircraft configuration design, mission analysis and weight estimation, and the evaluation of fundamental six-degree-of-freedom Aerodynamic characteristics. Students will develop the ability to perform conceptual aircraft design and aerodynamic performance analysis, establishing a solid foundation for the design and development of fixed-wing UAVs.