載熱固體 的英文怎麼說

中文拼音 [zǎi]
載熱固體 英文
thermofor
  • : 載Ⅰ名詞(年) year : 一年半載 six to twelve months; six months to a year; 三年五載 three to five ...
  • : Ⅰ形容詞(結實; 牢固; 堅硬) firm; hard; solid Ⅱ副詞1 (堅決地; 堅定地) firmly; resolutely 2 [書...
  • : 體構詞成分。
  1. The conclusions obtained as follows : firstly, the structure ' s free frequency is decreased by the reduction of the mechanical property of the material with the increasing temperature ; secondly the thermal stress produced by the temperature gradient may decrease or enlarge the structures natural frequency ; thirdly, the variety of natural frequency of the alloy structures effected by the heat effect apparently higher than that of the composite material structures

    最後,採用ansys程序分析了合金材料、復合材料的板、彈結構的振動特性。在不同的條件下,取得以下結論:升溫導致的材料機械性能下降都會降低結構有頻率,而溫度梯度產生的應力可能降低也可能提高結構的有頻率;金屬材料結構的有頻率受溫度的影響要比復合材料結構的有頻率受溫度的影響要明顯。
  2. Flow and heat transfer of mixture of solid media and biomass in inclined tube

    和生物質粉沿傾斜管流動和傳的計算
  3. Honeycomb ceramic has high surface and lighter weight. it is good at the heat insulation, so it is suitable for various kinds of catalyst carriers. it is widely used for automotive emissions control, stationary emissions control, chemical processing and refining industries

    蜂窩陶瓷材料具有比表面積大、隔性較好及重量較輕的特點,因此它適用於各種用途的催化劑,現已被廣泛應用於汽車尾氣凈化、定氣排放的凈化、化學工藝、精練工業等方面。
  4. An interpolation program is used to convert the fluent result data to the ansys load data. it is a new method to analyze turbine tip clearance. in this paper, some research of the numerical computation of the tip clearance of aero - engine is done, the parametric method is used and the research on the flow, heat and structure integration analyses is accomplished

    本文對渦輪機匣氣化分析方法做了研究,通過編制了荷轉換與施加程序,從氣計算模型中提取溫度場計算結果,並作為荷加入到耦合計算模型中,實現了高壓渦輪機匣的一化計算分析,為實現渦輪葉尖間隙的氣化分析打下了基礎。
  5. Based on the analysis of gas - solid multiphase catalytic reaction, the chemical reaction model is established. when the reaction is controlled by the chemical dynamic, the reaction rate is introduced by consideration of the adsorption and desorption effects. when the reaction is controlled by mass transfer, the diffusion coefficient is established which can present the flow rate increases in small reynolds domain ; for the internal diffusion, the internal diffusion coefficient is derived, and then the internal diffusion is coupled with chemical reaction to represent the phenomenon that the diffusion and the chemical reaction occur cocurrently

    本文在考慮催化轉化器內發生的傳傳質現象的基礎上,建立了催化轉化器的一維單孔道和三維多孔道傳傳質模型;在分析內以氣-多相催化反應為特點的工作機理的基礎上,建立了催化轉化器的化學反應模型:當催化轉化處于化學動力學控制區時,引入了考慮吸附、表面反應和脫附的表面化學反應速率公式,當催化轉化處于質量輸運控制區時,引入了決定外擴散能力的擴散系數公式和和決定內擴散速率的內擴散系數公式,並與化學反應速率相耦合,得出由擴散過程決定的化學反應速率公式。
  6. The response of solid rocket motor that exposed to the thermal load was simulated by use of the thermal conductivity equations with source term. the thermal hazard of solid rocket motor was evaluated. some measures to decrease thermal hazard of solid rocket motor has been put forward

    採用帶源項的傳導方程,對火箭發動機在遭受荷時的響應情況進行了數值模擬,有效地評估了在外界荷作用下發動機的危險性,並提出了減少發動機危險性的措施。
  7. According to the meso - scale structural characteristics of composite solid propellants ( csp ), the damage modes in csp induced by mechanical impacts, and the conclusions of former research, crack friction is considered to be the key factor for csp hot - spots

    本文根據推進劑細觀結構特徵及撞擊荷作用下的損傷破壞模式,結合相關理論分析結果,將裂紋摩擦作為推進劑點形成的關鍵因素。
  8. The research work of this dissertation aims at the study of srm safety under mechanical impact. based on mechanism analysis of hotspots and by use of dynamic finite element method, efforts are focused on the establishment of a general theory applied for srm safety analysis under mechanical impact

    本文對機械撞擊荷作用下火箭發動機安全性進行研究,以點機理分析為基礎,以結構動力有限元方法為手段,將點細觀模型與發動機結構撞擊變形分析有機結合,旨在探索機械撞擊荷作用下火箭發動機安全性分析研究的方法和途徑。
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