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


Advisor Professor Rimon Arieli
Advisor's Email rimonar@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 Geva Amit 2018 MSc Abstracts Investigation of a Morphing Wing Capable of Airfoil and Span Adjustment using a Retractable Folding Mechanism - New Engineering Approach
 2 Novikov Alina 2017 MSc Abstracts The Effect of Flow Bleed on the Starting Process of a Ramjet Engine Intake
 3 Nadler Zvi 2016 PhD Abstracts Effects of Low-Profile Vortex Generators on a Turbulent Boundary Layer
 4 Peker Avi 2015 MSc Abstracts Feasibility Study of a Medium/Long Range Ramjet Cruise Missile
 5 Raviv Sayag Michal 2015 MSc Abstracts Investigation of the Flow Field about a Plate with an Oscillating Bump
 6 Vaynshtein Alexander 2015 MSc Abstracts On the Flow Stability of a Sudden Opening Supersonic Intake
 7 Komkov Valeriya 2015 MSc Abstracts Design of a Circular to Rectangular Transition Duct for 2D Exhaust Tail Pipe
 8 Rokita Tomer 2015 PhD Abstracts Experimental and Numerical Investigation of the Subsonic Flow Field inside and near a Weapons Bay
 9 Mizrahi Idan 2013 MSc Abstracts On the Aerodynamic Characteristics of a Flapping Wing
 10 Yam Maor 2013 MSc Abstracts Wind-Tunnel Investigation of Two Dimensional Sails
 11 Ktalav Noa 2012 MSc Abstracts "Bump" as a Shock Control Device at Transonic Speeds
 12 Keren Yuval 2012 MSc Abstracts Tests on a Hovering Flapping Wing
 13 Tiomkin Sonya 2012 MSc Abstracts Analytical and Numerical Study of a 2D Membrane Wing in Subsonic Flow
 14 Haddad Arza 2012 MSc Abstracts Theoretical Evaluation of the Performance of a Boron Containing Gel Fuel Ramjet
 15 Basov Evgeny 2011 MSc Abstracts Static Aeroelastic Investigation of a Forward Swept Wing at Transonic Speeds
 16 Elimelech Yossef 2010 PhD Abstracts Flow Field about Airfoils at Reynolds Numbers between 5000 and 50000
 17 Maayan Alon 2010 MSc Abstracts The Effect of Fineness Ratio on the Pitch Damping Derivative
 18 Friedman Chen 2007 MSc Abstracts Numerical Investigation of Circulation Control

Last updated on: Friday ,November 15, 2019