Flow over an airfoil

  PROJECT TITLE: To simulate flow over a cylinder To run a baseline simulation and then to calculate the Reynolds number which then is increased by a factor of 20%, 40%, and 100% To create animations for pressure-velocity for all the three Reynolds numbers. THEORY AND INTRODCTION Reynold's number is an important dimensionless…

                                 simulating flow over a body to calculate the drag coefficient of a car body                                   …

OBJECTIVE Model the flow over a NACA0017 airfoil For the angle of attacks 0,2,4,6,8,10 compare the lift and drag forces   introduction:  Lift Lift, or downforce as its known in the motor racing world, is the force generated perpendicular to the direction of travel for an object moving through a fluid…

introduction:Thermal conduction is the transfer of heat internal energy by microscopic collisions of particles and movement of electrons within a body. The microscopically colliding particles, that include molecules, atoms and electrons, transfer disorganized microscopic kinetically and potential energy, jointly known…

Steady turbulent flow over a backward-facing step Tutorial path: • $FOAM TUTORIALS/incompressible/simpleFoam/pitzDaily  we shall investigate steady turbulent flow over a backward-facing step.using a custom mesh    Governing equations • Mass continuity for incompressible flow ∇• U = 0 …

objective: solve the 1D supersonic nozzle flow equations using the Macormack Method by implementing both the conservative and non-conservative forms of the governing equation.also: Figuring out the minimum number of cycles for which the simulation should be run in order for convergence Compararing the normalized mass flow…

the given ode of the damped oscillation is as follows to solve it  we first simplify it using  theta=x1; (d(theta))/dt= (dx_1)/dt =x_2; (d^2 (theta))/(dt^2 )= (dx_2)/dt; substituting we get: `(dx_2)/dt= -b/m x_2-g/L sin⁡(x_1)` also we know that  (dx_1)/dt =x_2     solving using ode45 in matlab…