thank u v much,but the link would help me only from ansys point of view.for which ineed to give the input parameters.i anyways appreciate your patience to answer my query
Homework Statement
a rectangular flat plate wing is considered for an aircraft.the aircraft needs to take off and land on a 1500 m long sea level runway and to cruise supersonically at mach no 2.5 at 8000 m altitude.assume aircraft weighs 16500kgf and max thrust of aircraft at sea level is 1/3...