Mechanical/Aerospace Design Optimization

ANAND AMRIT

*** ****** ***, **** ***, Ames, IA,**014

Ph. no: 515-***-****,

Email: *******@*******.***

EDUCATION:

****- **** **** ***** **********, Ames, IA, USA

Doctor of Philosophy. Aerospace Engineering, GPA: 3.6/4 2014-2016 Iowa State University, Ames, IA, USA

Master of Science, Aerospace Engineering, GPA: 3.5/4 2010-2014 National Institute of Technology, Rourkela, India Bachelor of Technology, Industrial Design, GPA: 3.5/4 FOCUS: Design Optimization

PROFESSIONAL EXPERIENCE: CFD Design Optimization, Spike Aerospace Inc., 2017- present Research & Teaching Assistant, Iowa State University. INTERNSHIP: Hindustan Aeronautics LTD, India. Design and manufacturing of Aircraft wings. Developed efficient methods of manufacturing process using high speed tools with help of CAD/CAM and CFD analysis. EXPERTISE: Computational Fluid Dynamics, DOE, CAD modelling, Multidisciplinary design optimization, High performance computing, robust design, FEA, Numerical methods, Manufacturing, PROJECTS:

• Cyclone Business Jet: Design optimization lead for a subsonic business jet.

• Boeing GoFly: University AIAA team, Design and build a personal flying device.

• Formula SAE: University Formula (SAE) team. Chassis design and fabrication lead.

• Human Powered Vehicle Challenge (ASME): Captain of the University team. Design and manufacture of a light weight vehicle powered by human.

TECHNICAL SKILLS:

Programming Languages: Matlab, Python, C/C++

CAD & CFD Software: Solidworks, Abaqus, Ansys, Catia, Star-CCM+, Fluent, Openfoam, Gridpro. Other software: Microsoft word, Microsoft Excel, Powerpoint. COURSEWORK: CFD, Incompressible flow, Finite element analysis, Optimization method, Large scale complex system, Fracture and fatigue, Multi-Disciplinary design optimization, Compressible flow. PUBLICATION:

• Design strategies for multi-objective optimization of aerodynamic surfaces, Engineering Computations.

• Efficient Multi-Objective Aerodynamic Optimization by Design Space Dimension Reduction and Co- Kriging, AIAA AVIATION Forum.

• Aerodynamic Design of the RAE 2822 in Transonic Viscous Flow: Single- and Multi-Point Optimization Studies, AIAA AVIATION Forum.

• Aerodynamic Design of a Rectangular Wing in Subsonic Inviscid Flow by Direct and Surrogate-based Optimization, AIAA AVIATION Forum.

• Rapid Multi-Objective Aerodynamic Design Using Co-Kriging and Space Mapping, AIAA SciTech Forum.

• Application of Multi-Fidelity Optimization Techniques to Benchmark Aerodynamic Design Problems, AIAA SciTech Forum.

• Adjoint-Based Nonlinear Output Space Mapping for Accelerated Aerodynamic Shape Optimization, AIAA SciTech Forum

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