Ajet aircraft is traveling at 260 m/s in horizontal flight. the engine takes in air at a rate of 53.3 kg/s and burns fuel at a rate of 3.63 kg/s. the exhaust gases are ejected at 317 m/s relative to the aircraft. find the thrust of the jet engine. answer in units of n.

Asquare 1m x 1m plate is shown below. all four of its edges are kept at 0 co. at t=0the temperature distribution is given by: y xtsins n75)=.a) using separation of variables determine the temperature distribution t(x,y,t)along the plate at any time t.b) discretize the heat conduction equation +=22222 txtusing a second-order centered difference scheme for the two second derivatives and a first-order forward euler scheme for the first derivative. using von neumann stability analysis, determine the stability criterion for the proposed discretization scheme in terms of , hand t. solve for the maximum allowable time step tmax