Berechung der Luftkrufte und Druckverteilung ar Flugzeugee mit Aussenisston bei Unter – und Uber-schallgoschwindigkeit

摘要

An ©slating computer program was used after some modifications to calculate pressures, forces, and moments acting on en aircraft with external -mounted stores. The program is a so-called panel-program that is the configuration of interest is replaced by a large number of small surface elements associated with one or more special types of singularity. The strength of these singularities is determined by the given boundary conditions. Ones the singularity strengths are known, velocities and pressures may be easily computed. This method seems to be successful for difficult interference problems.