Kalyan Dagamoori

adkaap@r.postjobfree.com Contact:+91-707*******

To demonstrate high level of responsibility and share my expertise in acquired during my course work in Space and Asnautical Engineering. My strong technical competence in 2D/3D CAD design tools will help the company achieve its goals and objectives.

Professional Competencies

Structural dynamics

Systems design and testing

Flight mechanics and controls

Proficient in CAD design tools

Keen on analysing requirements and gathering extensive knowledge through critical thinking.

Professional Experience:

Internship: DRDO

Position: Student intern

Performing design and analysis on a wing propeller.

Conducted analysis on the structure of the wing.

Manufacturing of the wing based on the efficiency of the obtained results

Education

Masters in Space and Aeronautical Engineering

Sapienza Universita di Roma, Roma (Italy)

Jan 2021

Principle subjects:

-Semester 1: Gas Dynamics, Space Flight Mechanics, Compressible Flows.

-Semester 2: Aerospace Structures, Space Missions and Systems, Space Propulsion.

-Semester 3: Combustion, Experimental testing of Aerospace structures, Space craft Design.

Bachelors in Aeronautical Engineering

May 2015

MLR Institute of Management and Technology India

Technical Skills

Languages

: C, C++

Modelling Software

: CATIA, 2D -AUTOCAD, Analysis - ANSYS

Operating Systems

: windows Xp/vista/win7

Communication skills

: Excellent written and verbal communication skills.

Publications:

•Published a journal on A Brief Study on Airship Using Aerospace, Electronics and Communication Applications.

•Published a journal on A Study and Brief Investigation on Invisibility of Air crafts (Vimanas).

•Published a journal on A Study and Design of Scram jet Engine Inlet by Using Computational Fluid Dynamics Analysis.

•Published a journal on An Effect of Elevator Deflection on Lift Coefficient Increment.

•Published a journal on Design fabrication and testing of flapping wings of Micro Aerial Vehicle (MAV). -IJERA

•Published a journal on Experimenting Non-Destructive Testing Techniques on Welding Joints -IJOER

•Published a journal on A Study and Brief Research on Electric propulsion Of Spacecraft and Rockets.

Certifications:

•Attended in national seminar held at IIST on "Unmanned Ariel Vehicle",Trivendram.

•Participated in "Artificial intelligence" workshop conducted by Aerotrix.

•Attended a seminar on Avionics conducted by Aeronautical Society of India.

•Certified in "DELTA Wing -Aeromodelling" held at IIST,Trivendram,India

•Participated in "CANSAT" workshop held at BITS PILANI-GOA,India.

Projects:

Title: DESIGN AND ANALYSIS OF ONE Ø PROPELLER at (DRDO-Defence Research and Development Organization).

Description: The objective of this project is to produce maximum thrust of 1000N rotating at 4000 RPM at higher speed". Diameter of propeller is restricted to 1000mm. Maximum power available is 40 KW. The propeller will be made using carbon fibre composite to make it lightweight. Propeller is one of the main components in an unmanned aerial vehicle which is responsible to produce thrust. The cross section of propeller blade is an aerofoil section which is typically varying from tip to hub in terms of chord or twist distribution.

There are many variables for designing the propeller such as pitch angle, flow angle, chord distribution at the blade span and twist distribution. Blade elements theory will be used for designing the propeller. The blade span is divided into number of cross-sectional elements and for each element thrust generated and torque required will be calculated and summed to find total thrust and torque for the propeller. For optimization of blade, these variables will be varied iteratively and optimum solution will be selected.

Title - MODEL AND ANALYSIS OF THE WING STRUCTURE

Description: The objective of the project is model and analysis of a wing structure to find the dynamic analysis and static analysis are minimum. A wing is an aerofoil, which has a streamlined cross-sectional shape producing a useful lift-to-drag ratio. A wings aerodynamic quality is expressed as its lift-to-drag ratio when the engine is fixed to the wing. The wing undergoes lots of vibration; we find the maximum values y using dynamic analysis by taking 10 different mode shapes and the maximum stress and minimum stress on the wing. We have considered 2412 aerofoil for modelling and we have used CATIA and ANSYS software for analysing.

Title -STELLAR POPULATION AND EVOLUTION WITH CUBESAT(SPEC).

Description: The main objective of the mission is to investigate and demonstrate the feasibility in resolving binary M-dwarf stars with a low-cost CubeSat mission. For the test mission, a reasonable set of targets has been selected from Hipparcos catalogue with known characteristics in order to comply with the possible performances of a low-cost CubeSat system. The main driving parameter of the design is the effective feasibility of the mission within la Sapienza possibilities in terms of know-how, manufacturing and costs. The design of the mission has been performed during the “Spacecraft Design” course held at La Sapienza University of Rome in order to reach the twofold objective of both proving that a similar scientific mission can be performed by a low-cost satellite and create an educational platform to involve and train students in the design of a CubeSat mission via a concurrent engineering approach.

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