הפקולטה להנדסת אווירונוטיקה וחלל בטכניון ע"ש סטיבן ב. קליין היא מרכז אקדמי ברמה עולמית לאוירונוטיקה ואסטרונאוטיקה, המוקדש ליצירה, הרחבה והפצה של רעיונות וידע במדעי התעופה והחלל.
פרס מקס ודזירה בלנקפלד לחדשנות פורצת דרך באווירונוטיקה. הפרס החדש יוקיר תרומות פורצות דרך בהנדסת אווירונוטיקה וחלל ויטפח שיתופי פעולה בין-לאומיים ארוכי טווח וחילופי ידע אקדמי.
Royi Shabtay | The velocity field inside spherical-cap rising bubbles was measured quantitatively by ray-traced, planar laser-induced fluorescence (PLIF) and shadowgraphy and then used to calculate scalar transport properties for bubbles of different Reynolds numbers.
Eliezer Azoulai | This study investigates the feasibility of classifying anti-tank threats, specifically Rocket-Propelled Grenades (RPGs) and Anti-Tank Guided Missiles (ATGMs), based only on their Radar Cross Section (RCS) characteristics. A comprehensive target RCS database was constructed using electromagnetic simulations, and radar tracking scenarios were simulated to generate dynamic RCS measurements under varying Signal-to-Noise Ratio (SNR) levels and carrier frequencies of 10, 20, and 40 GHz.
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.
Royi Shabtay | The velocity field inside spherical-cap rising bubbles was measured quantitatively by ray-traced, planar laser-induced fluorescence (PLIF) and shadowgraphy and then used to calculate scalar transport properties for bubbles of different Reynolds numbers.
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.
Royi Shabtay | The velocity field inside spherical-cap rising bubbles was measured quantitatively by ray-traced, planar laser-induced fluorescence (PLIF) and shadowgraphy and then used to calculate scalar transport properties for bubbles of different Reynolds numbers.