脫粘 的英文怎麼說

中文拼音 [tuōnián]
脫粘 英文
abhesion
  • 脫 : Ⅰ動詞1 （脫落） cast; shed; drop; fall off 2 （取下; 除去） take off; strip; cast off 3 （脫離） ...
  • 粘 : 粘動詞（粘附） glue; stick; paste; adhere to; bond
  1. Debonding was detected for hot water immersions.

    熱水浸泡后能檢驗出脫粘。
  2. Peeling analysis of unperforated honeycomb structure

    無孔蜂窩夾層結構脫粘剝離應力分析
  3. To simulate the quiescence and flying status of the motor, the ablation is calculated with different cavity width

    為模擬發動機靜止與飛行兩種不同狀態，本文對不同寬度的槽縫人工脫粘層的燒蝕進行了計算，對其進行了比較。
  4. Abstract : from the point of theoretical analysis, this dissertation provides the coupling calculation on the hot gas temperature field and ablation in the cavity between stress release boot and insulation of solid motors. through the calculation, some law of the ablation of the stress release boot is found

    文摘:從理論分析的角度出發，通過對人工脫粘層和絕熱層所構成的槽縫燃氣溫度場與燒蝕的耦合計算，得出了人工脫粘層的燒蝕規律。
  5. Hence, it is very significant to analyze the mechanism and extend law of interface debond of solid rocket motor

    因此，研究固體火箭發動機界面脫粘的機理和擴展規律，是固體火箭發動機結構完整性分析的重要課題。
  6. Interface debond between propellant and liner is a key form of failure of the structure integrity in the analysis of solid rocket motor

    在固體火箭發動機結構完整性分析中，襯層/推進劑藥柱粘接界面的脫粘是完整性被破壞的關鍵形式之一。
  7. After igniting the motor, the combustion gas coming into the debond cavity may expand the debond cavity, and make an additional combustion area and lead to larger load

    發動機點火后燃氣進入脫粘腔，使脫粘腔變形並獲得額外的燃燒面積，從而導致更強的載荷。
  8. Causation about interface debond are composed of two aspect of physics and chemistry, the main physical reasons are stress intensity and material damage near motor interface created under various work loads

    導致固體火箭發動機界面脫粘的原因包含物理的和化學的兩個方面，在各種工況載荷作用下發動機界面附近的應力集中及材料損傷是產生脫粘的主要物理原因。
  9. Because the propellant grain is viscoelastic material, the liner and adiabatic layer are also viscoelastic one, the interface debond problem is actually interface crack about elastic - viscoelastic or bi - viscoelastic materials. research about this problem relates to the knowledge of viscoelastic mechanics and interface fracture and combustion. numerical analysis method about interface debond on solid rocket motor is researched in this paper

    由於固體火箭發動機的推進劑藥柱是一種粘彈性材料，襯層和絕熱層也具有粘彈性性質，因此其界面脫粘問題實際上是彈性-粘彈性或雙粘彈性各向同性材料界面裂紋問題，對該問題的研究涉及到粘彈性力學、界面斷裂力學和燃燒學等相關學科。
  10. Currently, the main methods used to measure the fiber / matrix interface properties of composite were based on micro - mechanics, including single - fiber composites fragmentation test ( sfc ), micro - debonding technique, single - fiber pull - out test, and single - fiber push - out test, in which sfc was most widely used

    目前直接用來測定纖維增強復合材料界面力學性能的主要微觀力學方法有單纖維復合材料斷裂實驗（ sfc ） 、微脫粘方法、單纖維拔出法、單纖維頂出法，其中以單纖維復合材料斷裂實驗的應用最為廣泛。
  11. Here, fem is applied in the analyses of i ) fiber axial stress and interphase shear stress in fragmentation tests during initially applied strain, ii ) influence of temperature on the stress transfer across the interface, iii ) modulus and thickness of the interphase and their influence on interfacial stress transfer, iv ) interfacial debonding process, and v ) fragment aspect ratio, contact friction along the interface and their influences to the interfacial stress transfer efficiency

    在論文的這部分工作中，使用有限元法描述和分析了逐節斷裂試驗中初始應變下的纖維軸向應力和界面相剪切應力，溫度對界面應力傳遞的影響，界面相模量和厚度、纖維節長寬比、界面脫粘過程、界面接觸中的摩擦效應等因素對逐節斷裂試驗中應力傳遞的影響。
  12. Although numerical methods have frequently been used in the study of frc, theoretical analyses of such test methods as pull out tests and single fiber fragmentation tests, seemingly simple, remain to be challenging problems. problems arise when other factors are considered in connection with the various numerical models. these factors include nonlinearities in the properties and / or geometries of the materials, influences of such environmental conditions as temperature ( which is also to be studied in the present work )

    本論文正是針對以往研究中的不足，在對纖維增強復合材料破壞問題進行數值模擬的研究中，綜合考慮了纖維和基體材料的非線性效應、纖維和基體材料受外載發生大變形時的幾何非線性，以及纖維基體之間界面脫粘時接觸單元的非線性效應。
  13. The tendency of the simulated curves of pull out forces vs. displacements agrees well with experimental results, indicating the use and power of the present approach

    模擬出的抽拔力隨位移的變化曲線，能明確顯示出界面脫粘的開始、結束，以及完全脫粘后克服摩擦力的滑移過程，驗證了其應用的合理性。
  14. The results of numerical simulations and analytical solution show good accordance, except in the region near the fiber ends, where the shear - lag approach causes considerable discrepancy. next, to overcome the unrealistic assumption of perfect bonding, augmented - lagrange contact algorithm, element " birth - death " and fem are combined in the study of the partial debonding between fiber and matrix under pull out forces

    然而完全粘結的假設過于理想，與實際應用相差較大，因此，本論文將有限元法，接觸演算法和單元生死法結合起來，研究較大抽拔力作用下，纖維與基體之間發生的逐步脫粘的過程，所得到的抽拔力的變化結果，與試驗數據比較，較為一致。
  15. The above program in this paper has laid a theoretical foundation of the design of the stress release boot

    本文所採用的方法可供今後人工脫粘層的設計參考。
  16. Based on the ultrasonic prompting, series of experiments about indt still had been done. the defect of metirical include aluminium honeycom seeper, aluminium tole microcrackle, aluminium honeycom board disglue, aluminium board microcrackle etc. the defect signal was distlled and analysed

    在此基礎上，應用超聲激勵，對系列試件缺陷，包括鋁蜂窩積水、鋁金屬薄片微裂紋、板形鋁蜂窩脫粘、鋁板微裂紋，進行了紅外無損檢測實驗，對缺陷信號進行了處理和分析。
  17. Elastoplastic behavior of particle reinforced metal matrix composites considering the interfacial debonding

    有界面脫粘時顆粒增強金屬基復合材料的彈塑性性能分析
  18. Decohesion and sliding are enhanced thanks to the anisotropy if the graphite sheets at the interphase / matrix interface

    而3d - c sic中界面處熱解碳層的各向異性結構會促進界面層的脫粘和滑動。
  19. Then the change of shear stress in the interface is deduced in theoretical way after the fibers are disengaged and pulled out from concrete

    從理論方面計算了纖維受力后在脫粘和拔出過程中界面剪應力的變化。
  20. This kind of positive feedback may extend the debonded area and result in out of control of pressure on the firebox, or even the explosion of the motor

    這種正反饋可能使脫粘面進一步擴展，導致出現燃燒室壓力失控甚至發動機爆炸的災難性後果。
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