Results 131 to 140 of about 5,507 (169)
Some of the next articles are maybe not open access.
ТÑÑбоÑеакÑивнÑй двÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ Ñ ÑÑгой 120 кÐ
2022Тема вÑпÑÑкной квалиÑикаÑионной ÑабоÑÑ: «ТÑÑбоÑеакÑивнÑй двÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ Ñ ÑÑгой 120 кл.ЦелÑÑ ÑабоÑÑ ÑвлÑеÑÑÑ ÑазÑабоÑка ÑÑÑбоÑеакÑивного двÑÑ ÐºÐ¾Ð½ÑÑÑного двигаÑÐµÐ»Ñ (ТРÐÐ) Ñ ÑÑгой 120 кÐ
openaire +1 more source
Физика. ТолковÑй ÑловаÑÑ ÑколÑника и ÑÑÑденÑа
2007СловаÑÑ ÑодеÑÐ¶Ð¸Ñ Ð±Ð¾Ð»ÐµÐµ ÑÑÑÑÑи ÑеÑÑÑÐµÑ ÑÐ¾Ñ ÑеÑминов. ÐÑеобладаÑÑее болÑÑинÑÑво из Ð½Ð¸Ñ â ÑеÑминÑ, вÑÑÑеÑаÑÑиеÑÑ Ð² ÑазлиÑнÑÑ ÑÐ°Ð·Ð´ÐµÐ»Ð°Ñ ÐºÑÑÑа Ñизики ÑÑедней и вÑÑÑей ÑколÑ: в Ð¼ÐµÑ Ð°Ð½Ð¸ÐºÐµ, молекÑлÑÑ ...
openaire +1 more source
ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй ÑÑÑбоÑеакÑивнÑй двигаÑÐµÐ»Ñ ÑÑгой 160 кÐ
2023The final qualifying work presents the results of designing a two-circuit turbojet aircraft engine with a thrust of 160 kN, running on kerosene. The explanatory note contains: thermal calculation of engine parameters, gas dynamic calculation of axial compressor, calculation of combustion chamber parameters, calculation of turbine by root diameter and ...
openaire +1 more source
ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй ÑÑÑбоÑеакÑивнÑй двигаÑÐµÐ»Ñ ÑÑгой 90 кÐ
2021There're projection and drafting of gas-turbine engine, paraffin-oil worked, that's conversion of aircraft turbojet double-flow engine AL41F1 in this bachelor's graduate qualification work. The preliminary calorific calling engine, gas-dynamic ' calling compressor', combustion chamber's and turbine's have done.
openaire +1 more source
ÐаÑкеÑинг. ТакÑика и ÑÑÑаÑÐµÐ³Ð¸Ñ Ð¼Ð°ÑкеÑинга
2016СооÑвеÑÑÑвÑÐµÑ Ð³Ð¾ÑÑдаÑÑÑÐ²ÐµÐ½Ð½Ð¾Ð¼Ñ Ð¾Ð±ÑазоваÑелÑÐ½Ð¾Ð¼Ñ ÑÑандаÑÑÑ Ð¿Ð¾ ÑпеÑиалÑноÑÑи 080200 "ÐенеджменÑ". ÐаÑеÑиал позволÑÐµÑ Ð¿Ð¾Ð»ÑÑиÑÑ Ð¿ÑедÑÑавление о пÑедмеÑе маÑкеÑинга, вклÑÑÐ°Ñ ÐºÐ¾Ð½ÑепÑÑалÑнÑе знаниÑ,
openaire +1 more source
ТеоÑÐ¸Ñ ÑиÑка и моделиÑование ÑиÑковÑÑ ÑиÑÑаÑий
2012УÑебное поÑобие оÑÑÐ°Ð¶Ð°ÐµÑ ÑволÑÑÐ¸Ñ Ð¸ оÑвеÑÐ°ÐµÑ ÑовÑеменное ÑоÑÑоÑние ÑеоÑии ÑиÑка. Рнем оÑÑажаеÑÑÑ Ð¿Ð¾Ð»Ð¾Ð¶ÐµÐ½Ð¸Ðµ ÑиÑка в конÑепÑии ÑÑÑойÑивого ÑазвиÑиÑ, пÑоводиÑÑÑ Ð°Ð½Ð°Ð»Ð¸Ð· пÑиÑодÑ, иÑÑоÑников и ÑÑÑ
openaire +1 more source
Создание ÐÐТУ Ñ Ð²ÑÑокой ÑÑепенÑÑ Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑноÑÑи
2017ÐеÑÐ²Ð°Ñ Ð³Ð»Ð°Ð²Ð° назÑваеÑÑÑ: «ТеÑмодинамиÑеÑкий ÑаÑÑеÑ». Рней пÑедÑÑавлен ÑаÑÑÐµÑ Ð¿Ð°ÑамеÑÑов Ñикла, а Ñак же обоÑнованнÑй вÑÐ±Ð¾Ñ Ð¿Ð°ÑамеÑÑов двигаÑелÑ, ÑÐ°ÐºÐ¸Ñ ÐºÐ°Ðº ÑÑÐµÐ¿ÐµÐ½Ñ Ð´Ð²ÑÑ ÐºÐ¾Ð½ÑÑÑноÑÑи, ÑÑÐµÐ¿ÐµÐ½Ñ Ð ...
openaire +1 more source
ÐвÑÑ ÐºÐ¾Ð½ÑÑÑнÑй двигаÑÐµÐ»Ñ Ñ ÑоÑÑажной камеÑой ÑÑгой 75кÐ
2020In this bachelorâs graduate qualification work, the afterburning turbojet engine with a thrust of 75 kN was calculated. AL-31F was chosen as a prototype. The work includes the variant calculation of thermodynamic parameters, the choice of the optimal operating mode, the gas-dynamic calculation of the axial compressor, the calculation of the ...
openaire +1 more source
2023
This work is devoted to the design of a two-circuit engine with an afterburner, thrust 60kN. Tasks that were solved during the study: 1. Thermal calculation of the engine with the choice of the optimal option; 2. Gas dynamic calculation of the compressor; 3. Calculation of the combustion chamber; 4. Gas-dynamic calculation of a low-pressure turbine; 5.
openaire +1 more source
This work is devoted to the design of a two-circuit engine with an afterburner, thrust 60kN. Tasks that were solved during the study: 1. Thermal calculation of the engine with the choice of the optimal option; 2. Gas dynamic calculation of the compressor; 3. Calculation of the combustion chamber; 4. Gas-dynamic calculation of a low-pressure turbine; 5.
openaire +1 more source
СоÑÑоÑние и безопаÑноÑÑÑ ÑдеÑной ÑнеÑгеÑики в ÑÑÑане
2020Рданной ÑабоÑе ÑаÑÑмоÑÑено ÑовÑеменное ÑоÑÑоÑние ÑдеÑной ÑнеÑгеÑики в ÑÑÑане, пÑоведен анализ ÑоÑÑоÑÐ½Ð¸Ñ Ð±ÐµÐ·Ð¾Ð¿Ð°ÑноÑÑи ÐÐС в РоÑÑии, на пÑимеÑе комплекÑной безопаÑноÑÑи.
openaire +1 more source