DEVICE FOR PHYSICAL MODELING OF FLIGHT OF OBJECT UNDER INVESTIGATION

摘要

the invention u043eu0442u043du043eu0441u0438u0442u0441u00a0 technology u043cu0430u043du0438u043fu0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 thin flexible u0438u0437u0434u0435u043bu0438u00a0u043cu0438 is simulated u0434u043bu00a0 researched object. to improve the robustness of u0438u0437u043eu0431u0440u0435u0442u0435u043du0438u00a0 u00a0u0432u043bu00a0u0435u0442u0441u00a0 physical u043cu043eu0434u0435u043bu0438u0440u043eu0432u0430u043du0438u00a0 by u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 u0440u0430u0437u043du043eu043eu0431u0440u0430u0437u0438u00a0 configurations flat trajectories dwi u0436u0435u043du0438u00a0 researched object.this u0434u043eu0441u0442u0438u0433u0430u0435u0442u0441u00a0 the device containing a flexible conveyor movable element includes a pulley and u043fu0440u0438u0436u0430u0442u044bu0439 to input and output rollers, the sake deno - the arm mechanism with its rotation ring, axis is aligned with the axis of the lead u0448u043au0438u0432u0430 aeshnidae, input and output rollers installed on the the ends of the lead u0448u043au0438u0432u0430 aeshnidae, drive a u0440u0435u0433u0443u043bu00a0u0442u043eu0440u043eu043c speedfor the following limits u0440u0435u0433u0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 frequency u0432u0440u0430u0449u0435u043du0438u00a0 leading u0448u043au0438u0432u0430 formula that takes into account the frequency u0432u0440u0430u0449u0435u043du0438u00a0, diameter u0448u043au0438u0432u0430 gap, force, mass, and dr. lina flexible element and u043du0430u043fu0440u00a0u0436u0435u043du043du043eu0441u0442u044c u043fu043eu043bu00a0 aerodynamic u0441u043eu043fu0440u043eu0442u0438u0432u043bu0435u043du0438u00a0 environment u0434u0432u0438u0436u0435u043du0438u00a0 flexible element. 5).