method of measurement of loads acting on the wing of an aircraft in flight

摘要

method u0438u0437u043cu0435u0440u0435u043du0438u00a0 loads acting on the wing of an aircraft in flight, u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 measured u043au0440u0443u0442u00a0u0449u0438u0445 points and u043fu0435u0440u0435u0440u0435u0437u044bu0432u0430u044eu0449u0438u0445 forces through u0442u0435u043du0437u043e sensors placed in the transverse u0441u0435u0447u0435u043du0438u00a0u0445 on span wing and measuring bending moments through u0442u0435u043du0437u043eu0434u0430u0442u0447u0438u043au043eu0432, placed on the upper and lower u043fu043eu0432u0435u0440u0445u043du043eu0441u0442 u00a0u0445 wing in zones of the front and rear u043bu043eu043du0436u0435u0440u043eu043du043eu0432 wingconnected in u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 registering equipment, so that, with a view to u043fu043eu0432u044bu0448u0435u043du0438u00a0 accuracy u043eu043fu0440u0435u0434u0435u043bu0435u043du0438u00a0 u043du0430u043fu0440u00a0u0436u0435u043du043du043e - deformed u0441u043eu0441u0442u043eu00a0u043du0438u00a0 wing, u043au0440u0443u0442u00a0u0449u0438u0435 mo the cops and u043fu0435u0440u0435u0440u0435u0437u044bu0432u0430u044eu0449u0438u0435 force u0441u0435u0447u0435u043du0438u00a0u0445 wing u0438u0437u043cu0435u0440u00a0u044eu0442 by u0442u0435u043du0437u043eu0434u0430u0442u0447u0438u043au043eu0432 posted on the walls of the front and rear u043bu043eu043du0436u0435u0440u043eu043du043eu0432 to neutral u043eu0441u00a0u043c u043bu043eu043du0436u0435u0440u043e new angle of 45 to u043fu043bu043eu0441u043au043eu0441u0442u00a0u043c transverse cross-section wing.