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.
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.
Charles Touitou has been an MSc student in the Faculty of Aerospace Engineering since 2024 and currently works as an aerodynamics engineer at Elbit Systems.
Dr. Liraz Mudrik is currently a Postdoctoral Fellow in the Department of Mechanical and Aerospace Engineering at the Naval Postgraduate School. He received his Ph.D. in Aerospace Engineering (direct track) from the Technion–Israel Institute of Technology in 2023, where he also earned his B.Sc. (cum laude).
A PostDoctoral Seminar by Eyal Baruch:
As space missions such as solar sails, reflector antennas and solar arrays increase in size, their dynamics become ever more important, since large deflections can lead to efficiency loss, damage, or stability loss. The first step in addressing these problems is the accurate identification of system dynamics, most notably vibration mode shapes, natural frequencies, and damping ratios. However, these systems often cannot be tested at full scale prior to deployment, and numerical simulations may overlook key components, such as the correct damping mechanisms. This problem is further intensified by the complexity of carbon fiber thin shells, which serve as the fundamental building blocks of ultralight deployable structures. For such systems, classical similitude methods such as dimensional analysis (DA) are inapplicable, since parameters such as shell thickness and the stiffness matrix cannot be experimentally scaled.
Charles Touitou has been an MSc student in the Faculty of Aerospace Engineering since 2024 and currently works as an aerodynamics engineer at Elbit Systems.
Dr. Liraz Mudrik is currently a Postdoctoral Fellow in the Department of Mechanical and Aerospace Engineering at the Naval Postgraduate School. He received his Ph.D. in Aerospace Engineering (direct track) from the Technion–Israel Institute of Technology in 2023, where he also earned his B.Sc. (cum laude).
A PostDoctoral Seminar by Eyal Baruch:
As space missions such as solar sails, reflector antennas and solar arrays increase in size, their dynamics become ever more important, since large deflections can lead to efficiency loss, damage, or stability loss. The first step in addressing these problems is the accurate identification of system dynamics, most notably vibration mode shapes, natural frequencies, and damping ratios. However, these systems often cannot be tested at full scale prior to deployment, and numerical simulations may overlook key components, such as the correct damping mechanisms. This problem is further intensified by the complexity of carbon fiber thin shells, which serve as the fundamental building blocks of ultralight deployable structures. For such systems, classical similitude methods such as dimensional analysis (DA) are inapplicable, since parameters such as shell thickness and the stiffness matrix cannot be experimentally scaled.