Experience

CycloTech GmbH

• Austria
• Aviation & Aerospace
• 1 - 100 Employee

• Aerodynamics Engineer

  • Apr 2018 - Present

  Establishing methodology and strategy for meshing and simulations Driving the new designs and/or optimizing existing designs with the aid of CFD and the knowledge gained from the flow-field. Preparation and execution of wind-tunnel/test-bench Establishing methodology and strategy for meshing and simulations Driving the new designs and/or optimizing existing designs with the aid of CFD and the knowledge gained from the flow-field. Preparation and execution of wind-tunnel/test-bench



Airbus France S.A.S.

• France
• Investment Management

• Research Intern

  • Apr 2017 - Sep 2017

  High fidelity 3D simulations of unsteady aerodynamics (upper wing buffet) Establishing and validating the simulation strategies for the prediction of complex flow with strong non-linear behaviors (Unsteady aerodynamics) using high fidelity CFD methods (Z-DES). High fidelity 3D simulations of unsteady aerodynamics (upper wing buffet) Establishing and validating the simulation strategies for the prediction of complex flow with strong non-linear behaviors (Unsteady aerodynamics) using high fidelity CFD methods (Z-DES).



Altran

• Australia
• Construction
• 1 - 100 Employee

• Advanced CFD Engineer

  • Oct 2011 - Aug 2016

  Structure and unstructured mesh generation for external and internal fluid flow analyses. Methodology and process establishment for CFD simulations in solvers elsA and TAU. Aerodynamic data production, post processing and analysis of the results. Documentation of the analyzed results and publishing as per customer specific standards. Technical support to identify and solve problems and/or provide suitable workarounds. Development of automation tools in excel using VBA and in Linux using shell scripts. Major Projects: Aerodata production for Loads, Performance and Handling Qualities. Chimera Mesh Simulations (elsA): Deflected control surfaces, Icing effects, Anemo-Clinometry (PAM) and Global Motion analysis (PQR). Solar mesh generation for different A/c’s & configurations. Onsite engagements: Onsite Technical Focal Point for Aerodynamics team at Airbus Engineering Centre India May 2014 - Aug 2016 (2+ Years) Discussion with Airbus activity leads on inputs, workload and deadline. Onsite workload management between resources. Responsible for delivery, quality checks, weekly and monthly reporting. Co-ordination for additional workload/requirements Onsite Coordinator at Altran Sud Ouest, Toulouse, France Jul 2013 - Oct 2013 (4 Months) Identifying new work scope on various projects like meshing, CFD analysis and support. Coordination between Off-shore team and end customer on technical and project management. Show less



Aeronautical Development Agency

• India
• Defense & Space
• 700 & Above Employee

• Junior Research Fellow

  • Oct 2010 - Oct 2011

  Pressure recovery using Auxiliary Air Intake Doors on Intake diffuser Optimization of AAID to recover the pressure loss during takeoff phase in combat aircraft. Numerical simulations are carried out using FLUENT and validated with wind tunnel results. Pressure recovery using Auxiliary Air Intake Doors on Intake diffuser Optimization of AAID to recover the pressure loss during takeoff phase in combat aircraft. Numerical simulations are carried out using FLUENT and validated with wind tunnel results.



Indian Institute of Technology, Madras

• India
• Higher Education
• 700 & Above Employee

• Project Associate

  • Aug 2009 - Jul 2010

  Spin Investigation of Generic Trainer Aircraft and its Recovery Strategies Prediction of critical control inputs for nonlinear flight dynamic motion (eg. spin) using bifurcation analysis. Aircraft dynamics obtained are used to devise recovery strategies of non linear motion by numerical simulations on linearized model of 6DOF (degrees of freedom) equations. Spin Investigation of Generic Trainer Aircraft and its Recovery Strategies Prediction of critical control inputs for nonlinear flight dynamic motion (eg. spin) using bifurcation analysis. Aircraft dynamics obtained are used to devise recovery strategies of non linear motion by numerical simulations on linearized model of 6DOF (degrees of freedom) equations.