Sunday 6 April 2014

Details




Rameez Hamdule

Working at: Milestone PLM Solutions Mumbai

As: Design and Analysis Engineer

Studied at: Queen Mary University of London

Lives in: Mumbai (India)

Manufacturing and Analysis

-Experimental Studies on 0710 Supercritical Aerofoil

3D CAD Model of  Supercritical Aerofoil Prototype

Parachute Prototype Analysis

-Problem Based Learning (PBL)

Free body Diagram of a simple Parachute

Computational - Engineering

-Calculation of Stress Intensity Factor using Abaqus and Fatigue life

Selection of nodes for displacement extrapolation.


Optimisation of the turbo-fan engine

-Aero-Engine Gas turbine performance exercise

                                                                     A typical Cross-Section of a turbo-fan engine

Saturday 5 April 2014

Computational fluid dynamics

CFD: Viscous flow over a wing profile, turbulence modelling.

Spalart Allmaras
Spalart-Allmaras: Wing at 6* angle