## Modeling, Assembling and Drafting a Machine Vice using SolidWorks

Assembled  Machine  Vice:

Drafting:

(1)  Clamping  Plate:

(2)  Handle  Cap:

(3)  Handle:

(4)  Jaw:

(5)  Lock  Nut:

(6)  Moveable  Jaw:

(7)  Nut  M10:

(8)  Screw  Rod:

(9)  Screw:

(10)  Washer:

(11)  Vice  Body:

(12)  Machine  Vice:

### Part Assembling in NX Cad (Unigraphics) Jishnu Handique · 2018-09-08 08:41:26

(1)  Pipe  Vice:   (2)  Knuckle  Joint:   (3)  Screw  Jack:   (4)  Toy  Train  Model:   (5)  Socket  Spigot  Joint:   (6)  AirCraft  Model: &nbs Read more

### Sheet Metal and Surface Modeling in NX Cad (Unigraphics) Jishnu Handique · 2018-09-08 05:37:46

Sheet Metal Designs:       Surface Models:           Read more

### Simulation of Flow past a Cylinder for various Reynold's Numbers in SolidWorks Jishnu Handique · 2018-08-19 03:40:07

TAKEN INPUTS: Diameter = 0.04 m Length = 0.1 m Density of Air = 1.225 kg/m3 Dynamic Viscosity = 18.6e-6 Pa.sec at 20 Degree Celsius Reynold No. = 20, 40, 100 We know that, Reynold No. = (Density x Velocity x Diameter)/Dynamic Viscosity By applying above inp Read more

### Design and Analysis of a Centrifugal Pump in SolidWorks Jishnu Handique · 2018-07-08 15:21:32

Total  Number of Iterations  taken  for  Simulation  =  500   CUT  PLOTs  Obtained  for  Velocity: (A)  Outlet  Velocity =  10 m/sec:     (B)  Outlet  Read more

### Modelling and Simulation of Flow through a Flowbench in SolidWorks Jishnu Handique · 2018-07-08 04:37:42

Grid  Dependency  Test:  The Test is done at Valve Lift  =  0.001 m for three different Mesh SetUp.   Mesh SetUp:           (1)  Number of cells in X Axis  =  16     &nb Read more

### OpenFoam Simulation of Flow through a Backward Facing Step Jishnu Handique · 2018-07-04 17:32:01

Problem  SetUp: Velocity  =  0.05  m/sec Start  Time  =  0  sec End  Time  =  1  sec delta  Time  for  0.2  Graded  Mesh  =  0.00001  sec delta  Time& Read more

### Simulation of Flow over NACA AirFoil in SolidWorks Jishnu Handique · 2018-07-03 09:11:51

RESULTS Obtained:   (A) Angle of Attack = 0 Degree:     (B) Angle of Attack = 2 Degree:     (C) Angle of Attack = 4 Degree:     (D) Angle of Attack = 6 Degree:     (E) Angle of Attack = 8 Degree: Read more

### Simulation of 1D Supersonic Nozzle Flow using MacCormack Method in MATLAB Jishnu Handique · 2018-06-25 11:00:59

Governing Equations for Non-Conservative form: (A) Continuity Equation: (delrho)/(delt) = -rho(delV)/(delx)-rhoV((del(lnA))/(delx)) - V((delrho)/(delx)) (B) Momentum Equation: (delV)/(delt) = -V(delV)/(delx) - 1/gamma((delT)/(delx) + T/rho(delrho)/(delx)) (C) E Read more