Chandra Bhushan Singh

                                                                                                                                                                                                  Download Resume (PDF)

 

 

C-303, RP Hall of Residence
IIT Kharagpur

Kharagpur -721302, India

Phone:   (0091) 99329 00876
E-mail:  cbsingh05iitkgp@gmail.com
Web:   http://www.freewebs.com/cbsingh05_iitkgp/

                     

OBJECTIVE

          

To procure a summer internship in an establishment in the field of Aerospace discipline  which could provide me with a stimulating work environment and afford me opportunity to continuously learn and develop new perspective.

 

EDUCATION

  

  Year

Degree

Institute

Board

Subjects/Specialization

Result

Rank

2008

B Tech

Indian Institute of Technology, Kharagpur

IIT

Aerospace Engineering

8.06/10

6/32

2004

Class 12th

Chinmaya Vidyalaya,Bokaro

AISSCE.

Math, Physics, Chemistry,Biology

82%

---

2002

Class 10th

Jawahar Navodaya Vidyalaya

Bokaro

AISSE

Math, Science, English

86.6%

1/80

 

PROJECTS

 

·         Positivity of viscous discritization procedure for meshless solvers, under Prof. N.Balakrishnan, Aerospace engineering, CAD Lab IISc Bangalore. (Duration: May-June 2007)

                                  Finite volume-based computations are made for most of the computational domain, in a layer in the vicinity of the wall boundary, meshless solvers are used. These attempts are limited to inviscid calculations. Positivity is important to guaranty Robustness of viscous flow Solver. It has been found that meshless solvers suffer from a lack of positivity of viscous discritization akin to the finite volume method for Cartesian-mesh calculations. The project aimed at checking positivity of different discritization schemes available to solve Reynolds Averaged Navier Stokes equation

 

                                  The technique, called Stochastically Optimal Feedforward and Feedback Technique (SOFFT), directly descends from optimal control and in particular from Explicit Model Following Control (EMFC). Unlike the most used model following techniques, in SOFFT the feedforward and feedback control laws are designed independently of one another. This Control is to be implemented to Vehicles flying at high angle of attack. The technique uses modern control theory, Neural network concept and Bifurcation Technique

 

 

SKILLS

 
Software

 

 

ACADEMIC ACHIEVMENTS

 

TERM PROJECTS

 

 

 

EXTRA CURRICULAR ACTIVITIES & AWARDS

 

 

 

COURSES UNDERTAKEN

 

Departmental:

  • Introduction to Aerodynamics
  • Low Speed Aerodynamics *
  • High Speed Aerodynamics *
  • Introduction to aerospace Structures *
  • Aerospace Structural Analysis *
  • Dynamics for Aerospace Engineers#
  • Aerospace Structural Dynamics
  • Introduction to Propulsion system
  • Theory of Jet Propulsion *
  • Thermodynamics
  • Signals and Network *
  • Control System Engineering *#
  • Mechanics of Flight
  • Aircraft Stability and Control #

 

Others :

  • Computer Software (Algorithm )
  • Programming and Data Structure *
  • Computer Applications in Aerospace Engineering #
  • Basic Electronics *
  • Symbolic Logic
  • Transform Calculus
  • Numerical solution to ODE-PDE
  • Engineering Drawing and Graphics *
  • Operation Research #
  • Introduction to Manufacturing Process *
  • Electrical Technology *
  • Engineering Entrepreneurship #

 

#   currently studing courses

*  With Lab Component