摘要: The Symposium discussed the specific needs for dynamic stability information of aerospace vehicles, the form in which it should be presented and the various means of obtaining it. The modern aerospace vehicle is often exposed to u... 展开 The Symposium discussed the specific needs for dynamic stability information of aerospace vehicles, the form in which it should be presented and the various means of obtaining it. The modern aerospace vehicle is often exposed to unsteady, irregular or asymmetrical flow fields that may have significant effects on its characteristics of motion. This is caused by the fact that the flight envelope of a present-day military aircraft or missile often encompasses flight at high angles of attack, flight at non-zero sideslip angles and the ability to perform translational maneuvers. The Symposium included reports on new developments in wind-tunnel, flight test, and analytical techniques; motion analysis and non-linear formulations; and sensitivity and simulator studies. Specialists discussed a broad spectrum of approaches to determination of dynamic stability parameters. (Author) 收起