Amit Malse, M.Tech Aerospace Engg.

+91-758*******

add703@r.postjobfree.com

linkedin.com/in/amit-malse

Academic Background:

Degree Institute Year Result

M Tech Aerospace

(Aerodynamics)

IIAEM, Jain University,

Bangalore

2017-2019 8.91 CGPA

B.E. Mechanical

P.E.S. Modern College of

Engineering, Pune

2012-2016 64.02 %

Certified Courses:

Course Platform Year

Flying Car Nanodegree Udacity Aug 2018 – Dec 2018

Simulation using ANSYS (Level 3) Udemy Jan 2020

Clear and simple VMware certified associate (VCA-DBT) Udemy Feb 2020 Technical Skills:

Programming: Python, MATLAB, C++

Technical Design: ANSYS FLUENT, Solid works, Auto-Cad, Techplot 360, XFLR5, ANSYS Space Claim, VMware Vsphere 6

Languages: English, Japanese (N5 level), Hindi, Marathi Industrial experience:

Internship at CSIR-NAL, Bangalore:

Performed study ‘Characterization of wing-tip vortex formation and control’ in a low speed wind tunnel at the MAV division, NAL, Bangalore. Achieved 30% wingtip vorticity reduction using Hoerner type winglet along with wing-tip vortex generation plots from L.E. to T.E. on a light weight UAV designed by NAL.

2D and 3D vortex contour plots generated in ‘Techplot 360’ software, using the data gathered from ‘5-hole probe’ during the experiment. Projects:

UAV Autonomous GNC System Design:

Reduced total preparation time by 10% by designing a new simplified autonomous trajectory generation program (Autonomous guidance system) for aerial scanning project for an UAV in Python programming language, hence eliminating the requirement of external trajectory generation software.

Designed customized navigation and control system part of the Autonomous GNC architecture in C++ programming language for selected type of UAV, as MTech final year project individually.

Electromagnetic shock-absorber:

Improved shock absorption by 5-10% and comfort in this innovative electromagnetic shock-absorber design than conventional shock absorbers as a B.E. final year project.

Taking advantage of magnetic repulsion principle by using electromagnets along with precision sensor and a control system, this shock absorber provides adaptive control.

This innovation can be modified to give the user stiffness adjustment ability according to travel and road conditions, providing further increase in comfort.

Projects on ANSYS workbench:

Performed geometry generation, meshing, and analysis in ANSYS Fluent on different cases for given problem statements during the course

‘Simulation using ANSYS’:

Centrifugal compressor, Heat exchanger, Rotating cylinder case,

Simple FSI – fluid solid interaction case

Flow over an airfoil, wing.

Extra-curricular Activities:

Poster presentation on ‘Experimental characterization of wing-tip vortex formation and its control’ at the ‘SAROD international conference 2018’.

Contact this candidate