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a. 2013, Post Doctoral Experience (1 ½ year) from Institute for Plasma Research [IPR], Gandhinagar, India.
b. 2013, PhD (Metallurgical & Materials Engineering) from Malaviya National Institute of Technology [M.N.I.T.] Jaipur, Rajasthan, India.
c. 2008, M.Sc. (Physics) from Malaviya National Institute of Technology (M.N.I.T.), Jaipur, Rajasthan, India.
d. 2006, B.Sc. from Govt. College Ajmer, M.D.S. University, Ajmer.
I. Development of a novel multilayered thermal barrier coating (TBC) system for more efficient aircraft and gas turbine engines, NUST “MISiS”, Moscow, Russia. (Continue… Oct 2014 onwards )
II. Development of Tungsten (w) Vacuum Plasma Spray Coatings for Fusion Reactor (ITER) (Post Doctoral work at Institute for Plasma Research, Gandhinagar, India), 2013-14.
III. Development and Characterization of Plasma Sprayed Aluminum Based Nano Composite Coatings (Phd Thesis), 2013.
IV. CFD Modeling of The Flate Plate Air Heater (Master’s Thesis), 2008.
· Deputy Editor-In-Chief of Journal of Materials Science & Surface Engineering (JMSSE)
· REVIEWER of Journal of Surface Engineered Materials and Advanced Technology (JSEMAT)
· REVIEWER of British Journal of Applied Science & Technology (BJAST)
· REVIEWER of Advanced Materials Letters
· REVIEWER of Physical Science International Journal
· REVIEWER of American Chemical Science Journal
Life time member of The Materials Research Society of India (MRSI)
Indian Institute of Metals [IIM]
Post Doctoral Fellow at Institute for Plasma Research [IPR], Gandhinagar, India.
My present research work includes the development of a novel multilayered TBC system for more efficient aircraft and gas turbine engines by employment of rare earth oxides (CeO2 and Sc2O3) as zirconia phase stabilizers, and rare-earth zirconates with low thermal conductivity, high phase stability, thermal expansion coefficient (CTE) close to that of metal substrate, high hardness, low Young modulus and high toughness desired properties.
Science: New Materials
Field of science: Coating and Thin films technologies of their receiving
Research area: Development of a novel multilayered thermal barrier coating (TBC) system for more efficient aircraft and gas turbine engines
Objectives: To develop a high performance novel multilayered TBC system for more efficient aircraft and gas turbine engines having low thermal conductivity, high phase stability, thermal expansion coefficient (CTE) close to that of metal substrate, high hardness, low Young modulus and high toughness.
Different ceramic powders will be air plasma sprayed to produce TBCs for turbine engine applications.
All the coatings will be examined with microstructure studies with typical defects, such as pores, microcracks and splat boundaries.
Effect of sintering on coating microstructure (typical defects, such as pores, microcracks and splat boundaries
Examine Phase stability in as-sprayed coatings above high temperature (1300 °C and above)