rocket ramjet

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)騐裝置及測控系統(tǒng)組成、功能、技術(shù)指標(biāo)和可以開展的研究工作。

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詞組短語

短語

• 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)

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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)