An apparatus for controlling aerodynamic drag hypersonic aircraft

摘要

the device u0434u043bu00a0 u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 aerodynamic resistance u0433u0438u043fu0435u0440u0437u0432u0443u043au043eu0432u044bu0445 aircraft containing the nasal part of the system, the u0440u0435u0433u0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 u043fu043eu043bu043eu0436u0435u043du0438u00a0 u0441u043au0430u0447 this u0443u043fu043bu043eu0442u043du0435u043du0438u00a0 and system u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0, the fact that the system u0440u0435u0433u0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 leap u0443u043fu043bu043eu0442u043du0435u043du0438u00a0 implemented in the form of ultrasonic u043fu044cu0435u0437u043eu044du043bu0435u043au0442u0440u0438u0447u0435u0441u043au043eu0433u043e u0438u0437u043bu0443u0447u0430u0442u0435 u043bu00a0,placed in the fore part of the flush on its longitudinal axis in the vicinity of a critical point.