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Student Thesis Supervision
    
Thesis In Progress
- Masters
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Ashish Modi
“Development of Compact, Miniaturized Sensory Devices Engineered using Nano-Technology“, Started May 2002
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Nicholas Viscio
“Rocket Assisted Micro Powered Parachute (RAMPP) Concept”, Started August 2002
Doctoral
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Kim Jong Min
“Active Flow Control Concepts for Micro-Rotorcraft” Started March 2001
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Eric Lass
“Mutifunctional Structural Reinforcement Featuring Carbon Nanotube Thin Films”, Started January 2002
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Jonghwan Suhr
“A Cellular Automata Approach for Nano-Scale Computations”, Started August 2002
Post Doctoral
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Juntaek Ryoo
“On the Equivalence Between Cellular Automata and Molecular Dynamics Simulations ” Started July 2002
Doctoral Thesis Committee Member
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Hyungdae Lee
Course and Curriculum Development
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MEAE.4920 – Aerospace Structures and Controls Lab
Offered Spring Semester – Annually, 2 credit hours
A new undergraduate laboratory course was developed and taught for the very first
time in the spring semester of 2001. The primary emphasis of the laboratory was on
experiments related to lightweight structures, structural dynamics, and control
as it applies to aircraft, spacecraft and rotorcraft. Experiments include tensile testing of aerospace structural
materials, elastic instability investigations of columns under compressive
load, introduction to basic strain gage sensing techniques, structural
vibrations of cantilevered Euler-Bernoulli beams and introduction to basic
airfoil aerodynamics and aeroelastic interactions.
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MEAE.4200 – Rotorcraft Performance Stability & Control
Offered Fall Semester – Annually, 4 credit hours
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MEAE.6060 – Rotorcraft Performance Stability & Control
Offered Fall Semester – Annually, 4 credit hours
The existing course content was
upgraded with new course materials. These included advanced topics such as: unsteady aerodynamics and dynamic
stall, rotor wake structure modeling and experimental flow visualization as
well as rotorcraft vibration and acoustics. Student “seminars” were also
incorporated into the curriculum to enhance student participation and
involvement in the learning process.
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MEAE.4320 – Fixed Wing Design
Conceptual and preliminary design of a fixed
wing aircraft to satisfy given commercial specifications. Includes elements of
initial sizing and weights, geometry selection, aerodynamic design, propulsion
integration, stability and control, loads, structural design, manufacturability
and cost analysis. Writing intensive assignments and student presentations to
help develop communication skills and team-work.
Honors and Awards
In Fall 2001, Prof. Koratkar was awarded the “Curriculum Innovation Award”,
by the Office for Undergraduate Education at the Rensselaer Polytechnic
Institute for developing a micro-rotor test platform to support theory and
design classes related to aerospace engineering. To bridge the gap between
theory and practical implementation and provide the students greater confidence
in the capabilities as well as limitations of conventional modeling and design
tools “laboratory experiments” were added to the curriculum. The
students were asked to test a micro-rotor system at different rotor speeds and
blade collective pitch settings. Both conventional untwisted, rectangular
planform blades as well as advanced geometry rotor blades were tested. The
rotor thrust, induced power, profile power and figure of merit were
experimentally measured and compared with the predictions of momentum theory,
blade-element theory and lifting-line theory. These tests served to enhance the
student’s physical understanding and appreciation of the fundamental concepts that
govern aircraft flight.
Under
this program, five undergraduate students (Victor Maldonado, Nate Gray, Thomas
Cuomo, Michael Davis and Wei Zhang) and two high school seniors (Ryan DeMuth
and Halden Grossman) have worked in Prof Koratkar’s laboratory. Three
conference papers with undergraduate students as co-authors have resulted from
this project. One of Prof Koratkar’s undergraduate students, Victor Maldonado
won a prestigious General Electric Fellowship to continue work on the
Micro-Air-Vehicle test platform over the 2002 summer semester.
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