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* Strength and Structural analysis of a ladder foot step.

*Static Finite Element Analysis.

*Am performing a structural analysis to find maximum load bearing capacity of ladder foot step and also to verify the maximum  designated load of 3KN as well as it has to have a  factor of safety 2.5 and main the intention to find maximum stress acting area and redesign those area with respect to amount of deformation acting  on certain by optimising surface area at those regions.

VTOL_Bulkhead_and_Skin_Bodyand_Skin_Body_Sun27Dec20_0216PM_Profile_Manual_Revolve

BulkHead16_Wed23Dec20_0636AM_Ifr_1_JPhi_0To12_IzBulk_2_Frame_Stress_Analysis

Skin_Body_Sun27Dec20_0718PM_MyLines_Profile_Worked_But_Revolved_Manually

BulkHead16_Sat26Dec20_1042AM_Ifr_1_IzBulk_1_e_1_rL_5_cm_Full_Stress Non Linear

BulkHead16_Sat26Dec20_1042AM_0327PM_Ifr_1_JPhi_0To12_IzBulk_1_2_e_1_rL_5_3Pt75_with_Skin

BulkHead16_Sat26Dec20_1008AM_Ifr_1_IzBulk_1_rL_7.5_cm_Stress_Full_Linear

BulkHead16_Sat26Dec20_1008AM_Ifr_1_IzBulk_1_rL_5_cm_Stress_Full

BulkHead16_Wed23Dec20_0636AM_Ifr_1_IzBulk_1_Force_Stress_Analysis

BulkHead16_Thu24Dec20_0800PM_Ifr_1_JPhi_0To12_Frame_Full_NonLinear_Stress

BulkHead16_Thu24Dec20_0800PM_Ifr_1_JPhi_0To12_IzBulk_2_Frame_Full_Stress

BulkHead16_Wed23Dec20_0636AM_Ifr_1_IzBulk_1_Stress_Analysis

BulkHead16_Thu24Dec20_0800PM_Ifr_1_JPhi_0To12_IzBulk_2_Frame_Full_Non_Linear_Stress_P_L, Pressure and  Load

BulkHead16_Wed23Dec20_0636AM_Ifr_1_IzBulk_1_Load_Stress_Analysis 2 Constrained at the Top and Bottom Holes

BulkHead16_Wed23Dec20_0636AM_Ifr_1_IzBulk_1_zBulk_1_Load_Stress_Analysis_Full Constrained at the Top and Bot Holes

BulkHead16_Fri19Dec20_0413PM_Ifr_1_JPhi_0To12_IzBulk_1_2_Arcs_5_10_Com_No_Skin_Stress_Analysis

BulkHead16_Teu22Dec20_0410PM_Ifr_1_JPhi_0To12_IzBulk_1_Loft_0to12_Arcs_5_10_Com_No_Skin_Stress_Analysis

The engineering challenge is to predict how well the finished product will perform under real-world working conditions.
This involves considering stresses and deformation as well as a range of failure criteria. 
honeycomb Core is used in many applications like aircraft, buildings, etc.  in this particular simulation a honeycomb core is simulated against static structural by applying a load, pressure on different faces with different conditions such as cantilever or fixed beam.  
A most important analysis of this simulation is finding out of plane elastic modulus. Out of Plane analysis is done by applying load in a particular direction and finding deformation, stress, and strain in that particular direction.  Therefore three different times load is applied in x, y, and z-direction to simulate out plane analysis.  I here have taken two conditions first cantilever beam and the second is a fixed beam.
 It was very easy and interesting to simulate here and the time consumed was even less as compared to other software.

To analyze different aspects in a flexible pavement

What are tables good for, absolutely nothing

Stresses in a spring as it experiences loads

Structural analysis of ductile iron part.

To find the stress, strain and deflections at various points in a layer of the pavement.

To analyse different aspects of a Flexible Pavement

This is testing a shelf I designed for my 3D printer and other tools.

to simulate stress analysis for pre-AC stand

testing Structural strength of the aerial screw

Strange  days have found us, even stranger we linger around.

FEA - stress analysis of a connecting rod

Structural Stability and Lift generation of a box wing

Kingpin holder is an Vital Component in car's steering system, Our goal is to minimize the weight for a given known stress.  I am going to use Static Structural Finite Element Analysis to calculate the deformation and stresses.

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