Journal of Theoretical
and Applied Mechanics
28, 3-4, pp. 447-466, Warsaw 1990
and Applied Mechanics
28, 3-4, pp. 447-466, Warsaw 1990
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.