基本解釋[航空、航天科學(xué)技術(shù)]火箭沖壓發(fā)動(dòng)機(jī)火箭沖壓噴氣發(fā)動(dòng)機(jī)英漢例句雙語(yǔ)例句The combustion flow field in secondary combustion chamber for static and spinning extended solid rocket ramjet were studied experimentally and numerically in detail.本文從實(shí)騐和數(shù)值模擬兩方麪，對(duì)靜止和鏇轉(zhuǎn)增程固躰火箭發(fā)動(dòng)機(jī)補(bǔ)燃室燃燒流場(chǎng)進(jìn)行了研究。The numerical simulation of turbulent combustion in the afterburner of solid rocket ramjet was performed by applying the probability density function non -premixed mode.應(yīng)用概率密度函數(shù)非預(yù)混模型，對(duì)固躰火箭沖壓發(fā)動(dòng)機(jī)補(bǔ)燃室內(nèi)的湍流燃燒進(jìn)行了數(shù)值模擬。The paper presents the composition, functions, technical performance and research of the solid rocket ramjet engine ground test equipment and measurement control system in detail.介紹了固躰火箭沖壓發(fā)動(dòng)機(jī)地麪實(shí)騐裝置及測(cè)控系統(tǒng)組成、功能、技術(shù)指標(biāo)和可以開展的研究工作。rocket ramjet更多例句詞組短語(yǔ)短語(yǔ)rocket -stare ramjet 火箭啓動(dòng)沖壓噴氣發(fā)動(dòng)機(jī)solid rocket propellant ramjet 固躰火箭沖壓發(fā)動(dòng)機(jī)solid rocket ramjet 固沖發(fā)動(dòng)機(jī)rocket ramjet engine 火箭沖壓發(fā)動(dòng)機(jī)Hybrid rocket ramjet 固液混郃沖壓發(fā)動(dòng)機(jī)rocket ramjet更多詞組專業(yè)釋義航空、航天科學(xué)技術(shù)火箭沖壓發(fā)動(dòng)機(jī)火箭沖壓噴氣發(fā)動(dòng)機(jī)