Method of constructing an optimal airfoil hypersonic aircraft

摘要

A method for constructing an optimal airfoil hypersonic aircraft, comprising exposing at its surface using the optimization criterion, characterized in that an optimization criterion is used the ratio of the degrees of the coefficients of lift and drag forces on which are formed the optimum surface of an aircraft for solutions avoiding the problem of collisions, using numerical methods for solving the full Navier-Stokes equations, which determine the pa ionalnoe location bearing surfaces and form the bow of the apparatus with minimal thermal loads, where p - the ratio of the degrees of lift coefficient and drag forces, which characterizes performance indicator derived from the numerical solutions of differential quality of the game, - lift coefficient, defined as the ratio of lift to the velocity head and the characteristic area, - forces the drag coefficient, defined as the ratio of drag forces to a short tnom pressure and characteristic square.