Post Job Free

Resume

Sign in

Engineering Software

Location:
Nagpur, Maharashtra, India
Posted:
December 14, 2020

Contact this candidate

Resume:

Pradeep Badave

Pune, Maharashtra

adinsm@r.postjobfree.com

832-***-****

I have competed my B.E in Aeronautical Engineering. Providing wings to my career I am looking for jobs in my domain.

Willing to relocate: Anywhere

Personal Details

Date of Birth: 1998-12-22

Eligible to work in: India

Highest Career Level: Fresher

Industry: Aerospace & Aviation

Total years of experience: 0

Work Experience

Internship Training

IIT Bombay

May 2020 to November 2020

Simulation project on computing the airflow inside a empty room using OpenFoam software. Education

BE in Aeronautical Engineering

Tagore Engineering College, Anna University - Chennai, Tamil Nadu 2017 to 2020

DIPLOMA in Aeronautical Engineering

Acharya Polytechnic Bangalore - Bengaluru, Karnataka 2014 to 2017

Skills / IT Skills

• Positive approach.

• Smart worker, sincere& honest.

• Ability to learn new things.

• Good communication skills

• CATIA

• ANSYS

• Python

• Autocad

Languages

• English - Expert

• Hindi - Expert

• Marathi - Expert

Projects / Papers Presented

MANUPULATION OF SHOCK TRAINS USING TABS

https://www.ijert.org/manipulation-of-shock-train-for-underexpanded-jets-by-tabs text=It%20was

%20observed%20that%20elliptical,as%20compensation%20for%20thrust%20loss. March 2019

This paper presents the influence of tabs on shock trains of Underexpanded jet issuing through a convergent nozzle. The shadowgraph of flow is captured to have an insight of shock structure prevailed in Underexpanded jet. Tabs were attached diametrically opposite. Tabs used in the study were elliptical and perforated elliptical. The blockage ratio was 5%. Shadowgraph pictures were captured for tabs along and normal to the flow for nozzle pressure ratios (NPRs) of 3, 4, 5, 6 and 7. It was observed that elliptical tabs, highly distorts the shock train compared to perforated elliptical tabs. However perforated elliptical tabs are more influential to reduce noise level as well as compensation for thrust loss.

Aerodynamic effect of tall building over short building https://www.irjet.net/archives/V7/i6/IRJET-V7I61415.pdf June 2020

• This paper aims to clarify the aerodynamic effect of tall building over an adjacent small building through CFD analysis using Ansys Fluent software. The flow through the tall building creates a low pressure region behind it causing the suction effect. The suction effect in between the buildings leads to ventilation problem for the short building. During the high velocity winds, there may be chances of structural damage to the small building. The gap (distance) between the tall and small building plays major key role in deciding the safety parameters of the small building. The results shows that peak suction pressure (CP value of about -2.5) created on the top surface of tall building highly responsible for ventilation problem in small building



Contact this candidate