PRATHIK KUMAR DEVALLA

Aerospace Engineering graduate student from University of Dayton seeking an entry-level position in the field of Aerospace and Mechanical Engineering to apply and develop technical skills that contribute towards personal and professional growth. Demonstrated strong communication skills and proficiency in MATLAB, CATIA, ANSYS Fluent, ANSYS Icepak, MSC Nastran, HyperMesh, CREO, Cradle CFD and Solidworks flow simulation EDUCATION

University of Dayton Aug-2017 to May-2019 Dayton, OH MS in Aerospace Engineering

CGPA: 3.1/4

Projects: * Aerodynamic and Heat Transfer Analysis for Hypersonic Control Surfaces of lifting reentry vehicles

* Aerodynamic analysis of various Ahmed Body Configurations using computational tools SRM University Jul-2013 to May-2017 Chennai, India B. Tech in Aerospace Engineering

CGPA: 8.37/10

Projects: * Design and fabrication of a solar thermal propulsion system for sun synchronous satellite

-Runner-up for the Best Project Award

Relevant Coursework: Computational Fluid Dynamics, Finite Element Analysis, Aircraft Structures, Numerical Methods, Heat Transfer, Air Breathing Propulsion, Flight Dynamics, Fundamentals of Aerodynamics,Transonic Aerodynamics, Hypersonic Aerodynamics, Compressible Flow, Thermodynamics, Theory of Elasticity CONFERENCE PAPERS AND CERTIFICATIONS

* An Insight Of Electricity Generation From The Turbulence Of Sea Waves, ASME 2016 conference paper

* Generation Of Electricity From Tires Using Faraday’s Law, ASME 2016 conference paper

* Introduction to Electronics Cooling, Udemy Certification 2019 ENGINEERING WORK EXPERIENCE

Aerospace Intern at Fairtech Ltd. Bengaluru, India May 2016-July 2016 Internal load generation for a typical wing box was calculated using analytical and computational methods. MS Excel was used for the analytical method and MSC Patran/Nastran was used for the computational method. Stress analysis was performed for various structural elements such as stringers, skins, spars etc. Mechanical Engineering Intern at Tech Mahindra Bengaluru, India May 2015-July 2015 Stress analysis and Rear spar analysis was performed on the Bombardier Q400 using MSC Patran and Nastran. Basic aircraft structures problems like shear flow, moment distribution etc were calculated using MS Excel. SOFTWARE PROFICIENCY

CATIA, ANSYS Fluent, ANSYS Icepak, ANSYS ICEM-CFD, MS Office, MATLAB, Solidworks, Solidworks Flow Simulation, Ansys APDL, MSC Nastran, Hypermesh, CREO and Cradle CFD. Email: ac94w6@r.postjobfree.com,

Phone: 937-***-****

Address: 826, Bing Dr, Santa Clara, CA- 95051