MEASUREMENTS OF THE VORTEX WAKES OF A SUBSONIC- AND AnSUPERSONIC-TRANSPORT MODEL IN THE 40- BY 80-FOOT WIND TUNNEL

摘要

The rolling moment induced on aircraft models in the wake of a model of a subsonic transport and of a supersonic transport was measured as a function of angle of attack for several configurations. A description of the tests and a presentation and analysis of the data is given in this memorandum.