Przybliżone wyznaczanie charakterystyk aerodynamicznych skrzydeł o obrysie trapezowym w zakresie naddźwiękowym

We deal with the numerical computations of the preasure distributions aerodynamic coefficients for trapezoidal and rectangular wing planform in a steady supersonic flow. The Mach-line method has been applied [1]. The results of computations have been compared with those obtained other theoretical methods and experimental data. Good agreement has been ascertained.