06.1 - Flight Dynamics and Control (Control & Modelling)
AERODYNAMIC REQUIREMENTS ASSESSMENT OF CIVIL AIRCRAFT BASED ON AIRWORTHINESS PERFORMANCE
R. Wang¹, Y. Liu¹, M. Zhang¹; ¹Northwestern Polytechnical University, China
Flight performance defines an aircraft’s mission capability and is a key design objective. Deriving aerodynamic requirements from performance and airworthiness standards at the conceptual stage reduces iteration and accelerates early aerodynamic design. This paper establishes aerodynamic constraints derived from performance indicators and airworthiness regulations across key flight phases.
DOI: 10.71945/icas2026_0106