METHOD OF LIQUIDS AND GAS FLOW THROUGH THE USE OF TECHNOLOGY solitons

摘要

1.method u0441u043du0438u0436u0435u043du0438u00a0 hydrodynamic u0441u043eu043fu0440u043eu0442u0438u0432u043bu0435u043du0438u00a0 for laminar flow in the conduit section in any form by replacing the u0442u0440u0435u043du0438u00a0 u0441u043au043eu043bu044cu0436u0435u043du0438u00a0 in u043fu0440u0438u0441u0442u0435u043du043d oh, the flow friction u043au0430u0447u0435u043du0438u00a0, u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 in a continuous sequence of paired, a determined vortices with the axis of u0432u0440u0430u0449u0435u043du0438u00a0 u043fu0435u0440u043fu0435u043du0434u0438u043au0443u043bu00a0u0440u043du043eu0439 at the board u0434u0432u0438u0436u0435u043du0438u00a0 flow and u043au0430u0442u00a0u0449u0438u0445u0441u00a0 on streamby u0441u043eu0437u0434u0430u043du0438u00a0 u0434u0432u0443u0445u0441u043bu043eu0439u043du043eu0433u043e flow, which u0441u0442u0440u0443u00a0 environment in the central part (u043du0435u0432u043eu0437u043cu0443u0449u0435u043du043du044bu0439 flow at motion body in a stationary environment) has the speed of movements u043du0438u00a0 greater than the speed of u0434u0432u0438u0436u0435u043du0438u00a0 environment in u043fu0440u0438u0441u0442u0435u043du043du043eu0439 areawith the speeding u0434u0432u0438u0436u0435u043du0438u00a0 central jets (u043du0435u0432u043eu0437u043cu0443u0449u0435u043du043du043eu0433u043e flow) on speed u0434u0432u0438u0436u0435u043du0438u00a0 u043fu0440u0438u0441u0442u0435u043du043du043eu0439 stream functionally u0441u0432u00a0u0437u0430u043du043e thickness gap and from the conditions of the u043du0430u0445u043eu0434u0438u0442u0441u00a0;where d is the thickness of the external flow field of the flow in the u043fu0440u0438u0441u0442u0435u043du043du043eu0439;;r is the radius of the inner stream.;u - speeding internal streams over speed external flow;;- u0432u00a0u0437u043au043eu0441u0442u044c.;2. method for p.1, where u0434u0435u0442u0435u0440u043cu0438u043du0438u0440u043eu0432u0430u043du043du044bu0435 vortices u0441u043eu0437u0434u0430u044eu0442u0441u00a0 u0441u043eu043eu0441u043du044bu043cu0438 pipeline round or arbitrary u0441u0435u0447u0435u043du0438u00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that the internal conduit (u0441u0442u0440u0443u0439u043du0438u043a) u0438u043cu0435u0435 t the final length, and the external is infinite, which u0438u0441u043fu043eu043bu044cu0437u0443u044eu0442u0441u00a0 u0434u043bu00a0 u0444u043eu0440u043cu0438u0440u043eu0432u0430u043du0438u00a0 two flows: u043fu0440u0438u0441u0442u0435u043du043du043eu0433u043e that u043fu043eu0437u0432u043eu043bu00a0u0435u0442 organize continuous p u043eu0441u043bu0435u0434u043eu0432u0430u0442u0435u043bu044cu043du043eu0441u0442u044c pairs of vortices, and the central u0434u0432u0438u0436u0443u0449u0435u0433u043eu0441u00a0 u043bu0430u043cu0438u043du0430u0440u043du043e,the thickness of the jet u043fu0440u0438u0441u0442u0435u043du043du043eu0439 functionally according to paragraph 1 u0441u0432u00a0u0437u0430u043du0430 radius of internal flow and speed differential from the internal and u043fu0440u0438u0441u0442u0435u043du043du043eu0439 jets, fort u043cu0438u0440u0443u0435u043cu043eu0439 adjustable or fixed with u0441u0435u0447u0435u043du0438u00a0 entry in the external cavity u0441u0442u0440u0443u0439u043du0438u043au0430.;3. method for p.1, where u0434u0435u0442u0435u0440u043cu0438u043du0438u0440u043eu0432u0430u043du043du044bu0435 vortices in the u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 u0441u043eu0437u0434u0430u044eu0442u0441u00a0 pipe length, so that, with a view to u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 outlet pipes u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 range stream and u0443u043cu0435u043du044cu0448u0435 u043du0438u00a0 reactive force u0441u0442u0440u0443u0439u043du0438u043au043eu043c organized in a two stream: u043fu0440u0438u0441u0442u0435u043du043du044bu0439 that u043fu043eu0437u0432u043eu043bu00a0u0435u0442 form a continuous sequence of pairs of vortices. and the central, u0434u0432u0438u0436u0443u0449u0438u0439u0441u00a0 u043bu0430u043cu0438u043du0430u0440u043du043e,the thickness of the jet u043fu0440u0438u0441u0442u0435u043du043du043eu0439 functionally according to paragraph 1 u0441u0432u00a0u0437u0430u043du0430 radius of internal flow and speed differential from the internal and u043fu0440u0438u0441u0442u0435u043du043du043eu0439 jets, cat u043eu0440u0430u00a0 u0444u043eu0440u043cu0438u0440u0443u0435u0442u0441u00a0 adjustable or fixed with u0441u0435u0447u0435u043du0438u00a0 entry in the external cavity u0441u0442u0440u0443u0439u043du0438u043au0430.;4. method for p.1, where u0434u0435u0442u0435u0440u043cu0438u043du0438u0440u043eu0432u0430u043du043du044bu0435 vortices u0441u043eu0437u0434u0430u044eu0442u0441u00a0 u043du0430u0431u0435u0433u0430u044eu0449u0438u043c on u0434u0432u0438u0433u0430u044eu0449u0435u0435u0441u00a0 in stationary environment, the body flow environment, isolated from a thin layer of the same environment, move u0449u0438u043cu0441u00a0 on body with a lower speed than u043du0430u0431u0435u0433u0430u044eu0449u0438u0439 flow through u0444u043eu0440u043cu0438u0440u043eu0432u0430u043du0438u00a0 thin u0441u043bu043eu00a0 in flat u0441u0442u0440u0443u0439u043du0438u043au0435, the environment in which u043eu0431u0435u0441u043fu0435u0447u0438u0432u0430u0435u0442u0441u00a0 u0449u0435u043bu00a0u043cu0438 in front of him with adjustable or fixed with u0441u0435u0447u0435u043du0438u00a0,with the speeding u0434u0432u0438u0436u0435u043du0438u00a0 external flow over the speed u0434u0432u0438u0436u0435u043du0438u00a0 environment in u043fu0440u0438u0441u0442u0435u043du043du043eu0439 area functionally u0441u0432u00a0u0437u0430u043du043e thickness u043fu0440u0438u0441u0442u0435u043du043du043eu0433u043e flux at u0445u043eu0434u0438u0442u0441u00a0 of u0443u0441u043bu043eu0432u0438u00a0.;where is the number of u0440u0435u0439u043du043eu043bu044cu0434u0446u0430;;u - speeding u0434u0432u0438u0436u0435u043du0438u00a0 external flow over u043fu0440u0438u0441u0442u0435u043du043du044bu043c;;d is the thickness of the u043fu0440u0438u0441u0442u0435u043du043du043eu0433u043e flow;;- u0432u00a0u0437u043au043eu0441u0442u044c.