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Engineering Flight

Location:
Ahmedabad, Gujarat, India
Posted:
July 31, 2020

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Resume:

Patel Abhishek

Mobile No: +91-966*******

Email Id: adeznb@r.postjobfree.com

CAREER OBJECTIVE

To perceive a career in a renowned firm with dedicated efforts and to associate myself with an organization that gives me a chance to update my knowledge. In-depth knowledge of languages and development tools, seeking a position in a growth-oriented company where I can use my skills to the advantage of the company while having the scope to develop my own skills.

EDUCATION QUALIFICATION

2020: B.TECH Aeronautical Engineering from Parul University, Vadodara, Gujarat

CGPA:5.9

2019:July-September: Aerospace from Peoples' Friendship University of Russia (RUDN), Ulitsa Miklukho-Maklaya, 6, Moscow, Russia, 117198

2015: H.S.C. from Baroda Bagikhana School, Vadodara, GSHSE Board Gandhinagar.

2013: S.S.C. from Zenith High School, Vadodara, GSHSE Board Gandhinagar.

SUMMARY OF SKILL

Strong Mathemetical, analytical and problem solving skills.

Have knowledge regarding Wind Tunnel.

Having strong Awareness about the safety issues.

Manage multiple projects in a deadline-driven environment. Whether working remotely as a freelancer or as a full-time employee in an office.

Quick learner and willing to do hard work.

Efficient team player with abilities to work under any situations.

Increased knowledge of aircraft systems, flight test program procedures, documentation and regulatory requirements.

Served on team that conducted flight readiness reviews for new aircraft. Helped perform ground/electromagnetic interference tests, fit checks and remote site test preparations.

Gained competencies in a range of engineering disciplines and systems including structural design, aerodynamics, stress analysis, fluid power systems, fuel systems and test instrumentation.

ACADEMIC SKILLS DEVELOPMENT / TRAINING

Project Undertaken:

1)Enhanced Vegitation index mapping using landsat 8 satellite imagery:

We created a project regarding Landsat Surface Reflectance-derived Enhanced Vegetation Index (EVI) that are derived from Landsat 4 5 Thematic Mapper (TM), Landsat 7 Enhanced Thematic Mapper Plus (ETM+), and Landsat 8 Operational Land Imager (OLI)/Thermal Infrared Sensor (TIRS) scenes that can be successfully processed to Landsat Level-2 Surface Reflectance products. EVI is similar to Normalized Difference Vegetation Index (NDVI) and can be used to quantify vegetation greenness. However, EVI corrects for some atmospheric conditions and canopy background noise and is more sensitive in areas with dense vegetation. It incorporates an L value to adjust for canopy background, C values as coefficients for atmospheric resistance, and values from the blue band (B). These enhancements allow for index calculation as a ratio between the R and NIR values, while reducing the background noise, atmospheric noise, and saturation in most cases.

2)Flapping UAV:

The project has been created keeping in mind the Birds that can flap their wings to swoop, dive, glide, and alight on perches. Fixed-wing airplanes and rotary-wing helicopters rarely show that dynamism. Our purpose is then to build a numerical flight mechanics model that can be used in order to test and then to choose control strategies. As we are interested not only in cruise flight but also in stationary flight, we used an object approach for the common platform [16]: an exact mathematical formulation (with 6 dof) describes the kinematics of the articulated body (fuselage and two independent wings). The wing mass is neglected compared to the body mass: the mass centre is the central body one. The movements are calculated in a frame linked to the UAV, 4 angles being used for describing the wing movement (kinematics), the type of which can be very simply identified by: • ξ, is constant during a beat cycle and characterizes the stroke plane • λ, ν, µ vary during the beat cycle: λ defines the instantaneous stroke angle (flapping angle), ν is the rotation angle of the wing around its longitudinal axis (feathering angle) and µ represents the eventual lagging of the wing. For example, with ξ= 0, the stroke plane is vertical and with ξ= 90 it is horizontal.

Responsibilities:

1)Coordinated activities of technical engineers in the design, modification, and test of aerospace products.

2)Conceptualized designs for development of aeronautical products to meet customer requirements and aircraft design and purpose.

3)Conducted experimental, environmental, operational stress tests on models and prototypes of aircrafts and aerospace systems and equipment.

4)Conducted engineering research and analyzed data to determine feasibility, costs, and time of production.

Courses Undertaken:

1) Certificate for Completion of an independent Course of Study in Space Dynamics at Peoples' Friendship University of Russia (RUDN) .

2) Certificate for Completion of an independent Course of Study in Optimization Techniques at Peoples' Friendship University of Russia (RUDN) .

3) Certificate for Completion of an independent Course of Study in Remote Sensing at Peoples' Friendship University of Russia (RUDN) .

Computer SKILL

MS Excel, MS Project, Unix/Linux, Windows, Microsoft Word, PowerPoint Presentation, AUTOCAD

PERSONAL INFORMATION

Date of Birth / Age : 30th September 1996 / 23 Yrs.

Marital Status : Single

Nationality : Indian

Languages Known : English, Hindi, and Gujarati.

Address : A/26,Tirthak bunglows,kubereshwar Mahadev,Dabhoi Ring Road.

City : Vadodara.

DECLARATION

I the undersigned do solemnly affirm that the facts provided in this CV are true and genuine to the best of my knowledge & belief.

Patel Abhishek



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