Project Design

R.BHARGAV **************@*****.***

Mobile: +91-970*******

Career Objective:

To secure a challenging job with greater career prospects where I can learn and contribute to the growth of the company and increase my knowledge horizon and consulting capability.

•.

Educational Qualification:

B.Tech

S.V.Institute of Engineering & Technology, JNT University Hyd.

68%

May

2014

M.P.C

Sri Chaithanya Haritha Junior College, Board of Intermediate Education

53%

April 2010

S.S.C

Z.P.S.S High School, Board of Secondary Education

68%

March 2008

• Knowledge Summary:

•good knowledge eperince in creo parametric 2.0 3d model design,drafting,solid model,part design

• Creo parametric enables the creation of 3D parts, from 3D sketches, sheetmetal, composites, molded, forged or tooling parts up to the definition of mechanical assemblies.

Project Experience:

Project # 1

Role : Design and Analysis of Super Crtical Airfoil

Duration : 2013jan-feb(45days)

Project Description:

A supercritical airfoil is an airfoil designed, primarily, to delay the onset of wave drag in the transonic speed range. Supercritical airfoils are characterized by their flattened upper surface, highly cambered (curved) aft section, and greater leading edge radius compared with traditional airfoil shapes. The supercritical airfoils were designed in the 1960s, by then NASA engineer Richard Whitcomb,While the design was initially developed as part of the supersonic transport (SST) project at NASA, it has since been mainly applied to increase the fuel efficiency of many high subsonic aircraft. The supercritical airfoil shape is incorporated into the design of a supercritical wing.

Client Description:CATIA V5 Software in the areas of Structural Designing for R&D design solution and CAD /CAM training instittute in hyderabad .this projecr using design analysis software institute

Learned objects:

•I have using major desgining software catia airflow configuration.

•Supercritical airfoils feature four main benefits: they have a higher drag divergence Mach number.

•At a particular speed for a given airfoil section, the critical Mach number.

•created NASA airfoil using coordinates and high-speed.

•configuration of airfoil using drag divergence and super critical airfoil.

•completed airfoil desing a lower mach number.

•This makes the supercritical wing a favorite for designers of cargo transport aircraft.

Project Experience:

Project # 2

Role : Design Analysis of Transport Fuselage Structure

Project Type : Designing

Client : JET Wings, Hyderabad

Duration : January 2014 to March 2014

Project Experience:

The fuselage is an aircraft's main body section that holds crew and passengers or cargo. In single-engine aircraft it will usually contain an engine, although in some amphibious aircraft the single engine is mounted on a pylon attached to the fuselage which in turn is used as a floating hull. The fuselage also serves to position control and stabilization surfaces in specific relationships to lifting surfaces, required for aircraft stability and maneuverability.

Client Description:

Jetwings is the Authorized Training provider of CATIA V5 Software in the areas of Structural Designing for NATIONAL DESIGN RESEARCH FORUM, IEI, Bangalore. Jetwings is the Education & Training Group member of NAFEMS, India (Head quarter at U.K).from various organizations and Academic Institutions like NAFEMS, NAL, HAL, DRDO, Jet Airways, IIT’s and NIT’s.

Roles&Responsibilities :

•Providing the Support to the End Users for on-going daily operations.

•Assisting the End Users in Month End Closing.

•Daily Client interaction, understanding requirements and working on the same.

•interagating my team members and thinking project implementation.

•Holding weekend meetings with the associates in the team for any updates or feedback

Personnel Details:

•Father Name : Raavi Sathyanaraya

•Date of Birth : 31st Aug 1993

•Marital Status : Single

•Hobbies : Listening music, Playing cricket

•Languages Known : Telugu, English, Hindi

•Present address : H. No: 5-2,

Ghandhi Nagar,

Kukunoor Mandal,

Khammam District.

(I hereby declare that the information furnished above is true to the best of my knowledge)

Date: Yours sincerely

Place: (Raavi Bhargav)

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