Conjugate Heat Transfer Simulation

Objectives To simulate and analyse flow over NACA 2412 Airfoil and calculate drag and lift coefficients for different angle of attack as follows. Angle of attack = 1º Angle of attack = 5º Angle of attack = 10º Angle of attack = 15º also to simulate for different Turbulence model k-ω -sst RNG -k-ϵ…

Objectives To simulate and analyse flow over an ahmed body  To calculate Lift and Drag force coefficients Problem Description     The geometrical shape of the Ahmed body investigated is depicted in Figure 1 for inlet bulk velocity of 40 m/s. The body represents the basic aerodynamic properties of a…

Objectives To simulate and analyse flow over FSAE car for two cases Case 1:  Racing track conditions - Lot of turns Average lap speeds - 45kmph 70% turns at 45 degrees 20% turns at 80 degrees 10% turns at 20 degrees Case 2: Racing track conditions - Straights Average lap speed - 75kmph  Problem Description  …

Objective To simulate and analyse 2D open channel flow for backward facing step for 3 different mesh size for same geometry and same initial condition for 3 different cases. Case 1: dx = 2e-3m,              dy = 2e-3m,       dz = 2e-3m Case 2: dx = 1.5e-3m, …

Objective To Simulate and analyse conjugate heat transfer flow through circular pipe.  Problem Description A flow through pipe having internal diameter 0.03 mm and thickness of 0.005 mm is considered made up of aluminium is considered.The inlet Reynolds Number is 7000. Through outerwall of there is heat flux of -…

Objective To simulate and analyse Prandtl Meyer Shock flow Problem. In this case we have considered 2 cases. Case A : Initial velocity in region is supersonic (680 m/s) at 1 atm Pressure @ 300 K Case B : Initial velocity in region is subsonic (100 m/s) at 1 atm Pressure @ 300 K each case is simulated over 3 different…

Objective To simulate and analyse 2D open channel flow for 3 different mesh size for same geometry and same initial condition. Case 1: dx = 2e-4m,              dy = 2e-4m,       dz = 2e-4m Case 2: dx = 1.5e-4m,           dy = 1.5e-4m, …

Objective To simulate and analye flow over throttle body under Transient state condition. Here, for analysis we have considered total 5 cases using Transient solver. Case 1 : Pipe Flow Case 2 : No Throttle Case 3 : Throttle at 0 degree. Case 4 : Throttle at 25 degree. Case 5 : Throttle moving from 0…

Objective To Simulate and analyse flow through tube which occurs because of shock takes place in the tube due to suddent mixing of the two species kept at two different pressure. Problem Description A closed tube is considered in which the half part is occupied by N2 at 600000  pa and half part is occupied by O2 at …

Objective To simulate and analye flow over throttle body under steady state condition. Here, for analysis we have considered total 4 cases. Case 1 : Straight Pipe Flow Case 2 : No Throttle  Case 3 : Throttle at 0 degree. Case 4 : Throttle at 25 degree. Geometry The link for .stl file of geometry…

https://drive.google.com/open?id=1Er66WkvEOKPwH5NPnBv8MR3zp6mqbr1g