combustor pressure 中文意思是什麼
combustor pressure
解釋
燃燒室壓力-
Large - eddy simulation of pressure oscillations in a dump combustor
突擴燃燒室低頻壓力振蕩的大渦模擬 -
P33 - ng3 north american standard gas furnace ; combustor ; sit valve chamber ; electric pressure ignition ; ceramic simulation wood ; simulation ceramics ashes, safety mini crystal ceramics glass ; flame regulator
Ng3北美製式天然氣爐體；燃燒室； sit閥體；壓電點火器；陶瓷模擬木材；陶瓷模擬灰燼，微晶陶瓷安全玻璃；火焰調節器。 -
P48 - ng north america natural gas furnace ; combustor ; sit valve chamber ; pressure ignition ; ceramic simulation wood ; simulation ceramics ashes, straight safety mini crystal ceramics glass ; flame regulator
Ng北美製式天然氣爐體; ；燃燒室； sit閥體；壓電點火器；陶瓷模擬木材；陶瓷模擬灰燼，平直微晶陶瓷安全玻璃；火焰調節器。 -
And the experimentation has been done. it ' s primary results were given, such as temperature and pressure curve for the combustor and gasifier
並進行了多聯產方案試驗，給出了燃燒爐、氣化爐的升溫曲線、床層壓降曲線等初步試驗結果。 -
The results indicate that with the coefficient of residual oxygen being less than 1 or around 1, when the fuel is injected into the combustor at the same combustor pressure, the higher the combustor temperature is, the less the coefficient of residual oxygen is when auto - ignition occurs ; when the fuel is injected into the combustor at the same combustor temperature, the larger the combustor pressure is, the less the coefficient of residual oxygen is when auto - ignition occurs ; when the fuel is injected into the combustor at the same combustor temperature and pressure, the bigger the coefficient of residual oxygen is, the more easily auto - ignition occurs
研究結果表明，當推進劑處于余氧系數小於1或略大於1時，在燃燒室壓力相同的情況下噴入燃料，燃燒室溫度越高，可自燃的余氧系數越小;在燃燒室溫度大致相同的情況下噴入燃料，燃燒室壓力越高，可自燃的余氧系數越小;在燃燒室溫度、壓力大致相同的情況下噴入燃料，余氧系數越高，自燃發生的可能性越大。 -
The performance of supersonic inlet determines the pressure and the air flux in combustor, then affect the work of ramjet
超聲速進氣道的性能優劣決定了補燃室流場內的壓強和空氣流量，進而影響到沖壓發動機的工作性能。 -
The experimental results indicates that the secondary mass flow increases with increasing of primary mass flow rate, but the bypass decrease because the primary mass flow rate increase more rapidly than secondary mass flow. the expansion configuration shows low thrust property due to low pressure in flow path. the secondary nozzle changes the pressure distribution in ejector combustor, and decreases bypass ratio, but obtain more completely mixing
結果表明：二次流流量隨著一次流流量的增加而增加，由於二次流流量的增加速度低於一次流，引射系數減小；在純擴張式結構實驗中，引射燃燒室壓強很低，難以實驗推力增強；二次噴管改變了引射燃燒室的壓強分佈，降低了引射系數，改善了混合狀況能；對于本文的實驗結構，存在一個最優的二次噴管出口面積，使引射火箭推力最大，同數值模擬結果相吻合。 -
There are great differences between ground test of a flight vehicle ' s aerodynamics and that of a dual - mode scramjet when ground test facilities are used to do experiments on a dual - mode scramjet engine, the components of incoming flow and its parameters, including total pressure, total temperature ( or total enthalpy ) and velocity must be simulated. at the same time, since the fuel ' s resident time within a combustor is very short, on the order of one millisecond, it is difficult to measure the flow - fields
進行雙模態沖壓發動機地面試驗研究時，必須要求試驗設備能模擬實際飛行條件下來流氣體的組分、總壓、總溫（或總焓）以及來流氣體的流動速度；同時由於燃料在燃燒室內駐留的時間很短，一般為毫秒量級，從而使流場物理量的測定顯得非常困難。 -
Scramjet combustor may realize the subsonic - combustion mode and supersonic - combustion mode respectively based on the control of fuel in variable flight conditions. isolator has great effect on mode transition and preventing unstart of inlet. inlet can be unstarted by raising the back pressure result from chemical energy release in the combustor
計算研究表明，在相同的來流條件下，供油規律對燃燒室的工作模態有著重大的影響；在不同的來流條件下，可以通過調節供油規律使燃燒室分別實現亞燃模態和超燃模態；隔離段對防止燃燒引起的壓力升高對進氣道的干擾和燃燒室的模態轉換具有重要的作用。 -
The results indicate that with decrease of exit area of secondary nozzle, the bypass ratio is decreasing, and the static pressure in integrated ejector combustor is increasing, and mixing condition becomes better. there exists an optimal exit area of secondary nozzle to get maximum thrust of rocket ejector
結果表明：引射能力隨著二次噴管出口面積的減小而減小；整體式引射燃燒室壓強隨著二次噴管出口面積的減小而上升，混合隨之更為充分；存在一個最優的二次噴管出口面積，使發動機推力最大。
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