הטכניון מכון טכנולוגי לישראלXyz
הטכניון מכון טכנולוגי לישראל - בית הספר ללימודי מוסמכים 
Ph.D and MS.c Theses, since 1988.


Advisor Professor Arieli Rimon
Advisor's Email rimonar@aerodyne.technion.ac.il
Advisor's Home-Site  
No of theses 18
Department Aerospace Engineering
Department Web Site aerospace.technion.ac.il


No.   Student's Name Graduation
Year
Degree Abstracts Research Name
 1 Amit Geva 2018 MSc Abstracts Investigation of a Morphing Wing Capable of Airfoil and Span Adjustment using a Retractable Folding Mechanism - New Engineering Approach
 2 Alina Novikov 2017 MSc Abstracts The Effect of Flow Bleed on the Starting Process of a Ramjet Engine Intake
 3 Zvi Nadler 2016 PhD Abstracts Effects of Low-Profile Vortex Generators on a Turbulent Boundary Layer
 4 Avi Peker 2015 MSc Abstracts Feasibility Study of a Medium/Long Range Ramjet Cruise Missile
 5 Michal Raviv Sayag 2015 MSc Abstracts Investigation of the Flow Field about a Plate with an Oscillating Bump
 6 Alexander Vaynshtein 2015 MSc Abstracts On the Flow Stability of a Sudden Opening Supersonic Intake
 7 Valeriya Komkov 2015 MSc Abstracts Design of a Circular to Rectangular Transition Duct for 2D Exhaust Tail Pipe
 8 Tomer Rokita 2015 PhD Abstracts Experimental and Numerical Investigation of the Subsonic Flow Field inside and near a Weapons Bay
 9 Maor Yam 2013 MSc Abstracts Wind-Tunnel Investigation of Two Dimensional Sails
 10 Idan Mizrahi 2013 MSc Abstracts On the Aerodynamic Characteristics of a Flapping Wing
 11 Sonya Tiomkin 2012 MSc Abstracts Analytical and Numerical Study of a 2D Membrane Wing in Subsonic Flow
 12 Yuval Keren 2012 MSc Abstracts Tests on a Hovering Flapping Wing
 13 Noa Ktalav 2012 MSc Abstracts "Bump" as a Shock Control Device at Transonic Speeds
 14 Arza Haddad 2012 MSc Abstracts Theoretical Evaluation of the Performance of a Boron Containing Gel Fuel Ramjet
 15 Evgeny Basov 2011 MSc Abstracts Static Aeroelastic Investigation of a Forward Swept Wing at Transonic Speeds
 16 Yossef Elimelech 2010 PhD Abstracts Flow Field about Airfoils at Reynolds Numbers between 5000 and 50000
 17 Alon Maayan 2010 MSc Abstracts The Effect of Fineness Ratio on the Pitch Damping Derivative
 18 Chen Friedman 2007 MSc Abstracts Numerical Investigation of Circulation Control

Last updated on: Friday ,June 14, 2019