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.
Shavit Attar | This study demonstrates closed-loop control of the shock train leading-edge location in a dual-mode scramjet combustor using fuel-injection distribution as the control input. Experiments were performed in a direct-connect, cavity-stabilized combustor with distributed ethylene injection.
Saar Levi | Hypergolic propellants are defined by their ability to ignite immediately upon contact, resulting in rapid exothermic reactions occurring without the need for an external ignition source. In hybrid rocket engines, this spontaneous reaction simplifies thruster management, reduces system mass, and enables engine re-ignition.
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.
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.
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.