MSNBC Space News
Wed, 8 Feb 2012 17:13:02 GMT
The most detailed image yet of the well-known Carina nebula has been caught by a European telescope, unveiling previously hidden features of an exquisite star nursery.
Wed, 8 Feb 2012 21:58:42 GMT
There are two interesting meet-ups in space for skywatchers this week: close encounters between the moon, several planets and stars.
Wed, 8 Feb 2012 20:31:35 GMT
A small newfound galaxy with an oddball shape may be the product of a close encounter with a neighboring galaxy in what scientists are calling a "stealth merger," a new study reveals.
Wed, 8 Feb 2012 02:44:18 GMT
Science editor Alan Boyle's blog: Colorful videos prove that the astronauts aboard the International Space Station had the best seats in the house for last month's northern lights.
Wed, 8 Feb 2012 01:36:55 GMT
A bright fireball streaked across the nighttime sky over eastern Texas and Oklahoma last week, and was caught on video by a police car camera.
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    CV: PhD Researcher (Aeroengine design and performance)

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    Personal information
     Name:<withheld>
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    Contact information
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    Candidate Profile
     Date Submitted:18-03-2010
     Last Modified:01-09-2011 (02:27)
    Job information
     Current job:PhD Researcher (Aeroengine design and performance)
     Employment Term:Permanent
     Job location:Anywhere
     Date available:immediately
     Industry:Civil Agencies/International Organizations, Satellite Manufacturers and Subcontractors, Satellite Operators, , , Launch Systems, Business Services
     KeywordsGas turbine design and performance Integrated Vehicle Health Management (IVHM) Aerospace materials Stress engineering Rocket Propulsion Aircraft design MATLAB Satellite Propulsion Aeronautical engineering
    CV

    PROFESSIONAL PROFILE

    A versatile professional seeking a challenging role in technology design & management and apply my experience of multidisciplinary engineering to provide excellent solutions.

    WORK EXPERIENCE:

    RESEARCH FELLOW, Design System Project Lead – Cranfield-BOEING IVHM Centre, Cranfield University, UK: FEB 2010 – CURRENT

    Technology development responsibilities:

    ·  Undertake parametric design, analysis of low bypass turbofan engine serpentine nozzle and computational analysis of designed nozzle.

    ·  IVHM Design system –Generic end to end solution architecture for Integrated Vehicle Health Management. Use cases for Rolls Royce and BAE Systems were used for validations.

    ·  IVHM design for BAE System Warship integrated with Rolls Royce power plant.

    ·  Implementation and modification in design tools and methods, eg QFD, MADe, PICAM and SHOAM (IVHM tool set for BOEING)

    ·  IVHM functionality systems and system implementations for existing EHM tools like Total care for Rolls Royce.

    Project Management responsibilities:

    ·  Project Management of aircraft advanced technologies. Prepare statement of cases, sanctions and financial concurrence for sponsored projects.

    ·  Plan, organize and carry out technical review of outsourced work. Ensure compatibility and security of data transfer of sensitive material.

    ·  Assist in preparation of task schedule for technology specific directorates. Organize regular weekly reviews of design teams.

     

    RESEARCH ASSISTANT – National high temperature surface engineering centre – High temperature corrosion laboratory – Surface science and engineering centre - Department of Engineering Materials, Cranfield University, UK.: May 2009 – Jan 2010

    • Accelerated Furnace Cyclic Testing (AFCT) & salt accelerated Oxidation testing for high temperature alloys used in hot sections of Aero-engines (Rolls Royce).
    • Development of thermal barrier coating for space applications – Tribological analysis
    • High Pressure Fatigue testing and analysis for stressed turbine discs and blading
    • Development of Plasma-based coating deposition and surface treatment technologies
    • Development of TBC for filtering unit of rocket motors
    • Wear behaviour of high performance materials - High temperature degradation mechanisms

     

    PROJECT ENGINEER – (MECHANICAL / AERONAUTICAL) - BHR Group –The Fluid Engineering Research Centre – Cranfield University, UK: SEP 2008 – MARCH 2009

     

    ·            Stress analysis of Aircraft Structures – Static stressing for turbo machinery bladin fuselage and wing structures. Roughness and impulse testing - Aircraft landing gears

     

    ·            Stress field analysis for aero structure, modelling of crack growth, crack arrest and fatigue

     

    ·            Safe Life Structural Design Criterion Analysis for structural failures which occurs in aircraft wings, propeller blades and engine discs

     

     

    ISRO SATELLITE CENTRE (ISAC), Indian Space Research Organisation (ISRO), BANGLORE,

     

    INDIA – INTERNSHIP – JAN 2006- APRIL2006

     

    ·           Developing satellite technology and implementation of satellite systems for scientific, technological and application missions.

     

    ·         Inter-planetary space mission shifting – Mission modelling

    LIQUID PROPULSION SYSTEMS CENTRE (LPSC), Indian Space Research Organisation ISRO, BANGALORE INDIA - INTERNSHIP -, OCT 2005- JAN 2006

     

    ·           Research was focussed on study of Earth Storable and Cryogenic propulsion, stages, associated control systems and components for Launch Vehicle and Spacecrafts.

     

    ·           Liquid propulsion risk assessment

     

    EDUCATIONAL BACKGROUND & EXPERIENCE:

     

    PhD RESEARCHER – AEROENGINE NOVEL PROPULSION SYSTEM DESIGN & PERFORMANCE

     

    DETERIORATION MODELLING – TECHNO ECONOMIC RISK ANALYSIS (TERA) DEPARTMENT OF PROPULSION, CRANFIELD UNIVERSITY, Jan 2008 – PRESENT

     

    ·         Invention and generation of stochastic probabilistic distributions to predict aero propulsion performance characteristics

     

    ·         Analysis of the aero/thermal requirements for Gas Turbine components

     

    ·         Preliminary and final design studies for Turbo-machinery (Compressor & Turbines)

     

    ·         Design methodologies for greener efficient combustors

     

    ·         Development of Techno-economic risk assessment (TERA) framework to predict possible optimized technology selection

     

    ·         Analysis of the aero/thermal requirements for Aero-engines for predicting performance

     

    ·         Aircraft trajectory optimizations & multi-disciplinary design optimisations (Boeing)

     

    ·         Design, planning and implementation of new concepts for Aero-engines (Open rotor Detonators)

     

    ·         Worked closely with Rolls Royce, AIRBUS, P&W and few leading European universities

     

    MSc – AEROSPACE MATERIALS, DEPARTMENT OF ENGINEERING MATERIALS, UNIVERSITY OF SHEFFIELD, SEP 2006 – SEP 2007 (DISTINCTION)

     

    ·         Individual Research Project based on design, manufacturing and testing for unique concept Self healing composites for aerospace applications sponsored by AIRBUS.

     

    ·         Group design project focused on stress field modelling of material for Aero-engine Integration

     

    ·         Finite element analysis & modelling was extensively used for this research project. analysis was employed to look at the bulging and fatigue crack growth behaviour fuselage pressure bulkhead and wing structures (FEM, CATIA)

     

    ·         Research study was conducted to understand the impact of nanotechnology for detecting early initiation of cracks in advanced engineering materials.

     

     

    BTech– AERONAUTICAL ENGINEERING, UNIVERSITY OF BOMBAY, INDIA,SEP 2002- Aug 2006 - (DISTINCTION)

    ·         Research thesis was focussed on developing novel Ion - Solar propulsion systems shifting space activities from one planet to other using Unmanned Space Vehicle.

     

    ·         Group design project - Estimation of contact conductance for nuclear fuel bundles in Reactor for Aviation Fuel. All the experimentations were carried on at Baba Atomic Research Centre, Mumbai, India.

     

    ·         Leakage characteristics, heat transfer operations and fluid interaction impacts were modelled and analysed. CFD modelling was used for heat flux flow patterning.

     

    COMPUTER SKILLS:

     

    •       Design Tools & Languages: MATLAB, C++, VB, CATIA, CFD, FEA

     

    •       Proficiency in MS-Office (Word, Excel, Access, PowerPoint), VBA


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