הפקולטה |להנדסת אוירונוטיקה וחלל

Yishai Glam | The aeroelastic stability and dynamic response of thin panels are important considerations in aerospace structures design. Traditional nonlinear Rayleigh-Ritz (RR) analysis struggles when applied to panels with nonuniform boundary conditions (BCs) or local constraints. Generating the necessary global basis functions is difficult, often leading to slow convergence and requiring many modes.

Bar Gawi | Hypersonic gliding vehicles (HGVs) operate in flight regimes characterized by nonlinear dynamics, significant aerodynamic uncertainties, and strong coupling between vehicle motions. These characteristics pose challenges for flight control design, particularly when tracking performance must be maintained despite model inaccuracies, changing flight conditions, and practical implementation limitations.