流體動力噴射 的英文怎麼說

中文拼音 [liúdòngpēnshè]
流體動力噴射 英文
hydrodynamic jetting
  • : Ⅰ動1 (液體移動; 流動) flow 2 (移動不定) drift; move; wander 3 (流傳; 傳播) spread 4 (向壞...
  • : 體構詞成分。
  • : Ⅰ名1 (力量; 能力) power; strength; ability; capacity 2 [物理學] (改變物體運動狀態的作用) forc...
  • : 噴動詞1. (液體等受壓力而射出) spurt; spout; gush; jet 2. (噴灑) spray; sprinkle
  • : Ⅰ動詞1 (用推力或彈力送出) shoot; fire 2 (液體受到壓力迅速擠出) discharge in a jet 3 (放出) ...
  • 流體 : [物理學] fluid; fluor流體力學 fluid mechanics; hydromechanics; 流體生物學 hydrobiology; 流體運動學 hydrokinematics
  1. The characteristics of high pressure gyratory sprayed pumping discusses is presented, which is applicable in wide range of scope and ground layers, convenient for construction, long durability, wide source of materials. mechanism for subgrade strengthening : complex foundation of cement solid and earth between piles was formed by pulsant load of flowing pressure and spraying flow, water wallop, cavitation phenomenon, water wedge effect, extrusion force and air flow agitation etc so as to enhance foundation bearing force and reduce settlement and deformation

    高壓旋注漿技術具有適用范圍、適用地層較廣,施工方便,耐久性好,材料廣闊等特點;其加固地基機理主要是通過壓、的脈負荷、水塊的沖擊、空穴現象、水楔效應、擠壓、氣等效應形成水泥固結與樁間土的復合地基,從而提高地基承載,減少沉降變形。
  2. Topics include : planets, planet formation ; stars, the sun, " normal " stars, star formation ; stellar evolution, supernovae, compact objects ( white dwarfs, neutron stars, and black holes ), plusars, binary x - ray sources ; star clusters, globular and open clusters ; interstellar medium, gas, dust, magnetic fields, cosmic rays ; distance ladder ; galaxies, normal and active galaxies, jets ; gravitational lensing ; large scaling structure ; newtonian cosmology, dynamical expansion and thermal history of the universe ; cosmic microwave background radiation ; big - bang nucleosynthesis

    課程的主題包含了:行星、行星形成;恆星、太陽、正常的恆星、恆星形成;恆星演化、超新星、緻密天(白矮星、中子星及黑洞) 、波霎、雙x -線源;星團、球狀及疏散星團;星際介質、氣、塵埃、磁場、宇宙線;距離階梯;星系、正常及活躍星系、;重透鏡;大尺度結構;牛頓宇宙學、宇宙的膨脹及溫度發展歷史;宇宙背景微波輻;大霹靂核合成。
  3. The ejected coolant interacts with the external flow near the endwall and generates aerodynamic and thermodynamic losses in the process. this reduces turbine stage efficiency and together with the consumption of cooling air is detrimental to the overall cycle efficiency

    但這種方法中的冷空氣與端壁附近的外場相互作用產生氣和熱損失,並且消耗冷卻空氣,從而損害渦輪的整循環效率。
  4. This paper analyzes the forming principle, effecting factors and controlling measures of poisonous gas of exhaust emission from petrol engine for vehicle fully and accurately. after the comparison on the emission control measures, it is clear that there is a trade - off relation between emission control and power, torque, fuel consumption of engine. " efi + catalytic converter " is a integration measure of in - engine and out - engine, which is a mainstream technology of emission control for petrol engine for vehicle

    本文通過大量的文獻閱讀,翔實的分析了車用汽油機排氣中有害氣成分的產生機理、影響生成的主要因素、治理排氣污染物的主要技術措施,指出這些措施與發機的其他性能(如性、經濟性等)的一種折中關系,只有「電控+排氣催化轉化」是一種機內與機外相結合的措施,是控制車用汽油機排放的主技術。
  5. The shearing layer is carried by the jet and the eddy is formed because of the instability and selective amplification of shearing layer which will propagate to the downstream. as the eddy impacts the impinging wall, a wave of pressure disturbance with certain frequency is induced. this wave then propagates to the upstream with high speed, and results in the overlap and amplification of the waves when the frequencies of them are close with each other

    當前束中的不穩定擾波在穿過腔內的剪切層時,剪切層對其有選擇放大作用,形成渦環結構,剪切中渦環與碰撞壁撞擊,在碰撞區域產生壓波並向上游反,在上游剪切層分離處誘發新的擾的產生,當新擾與原擾匹配時,上游就被不斷地受到周期性激勵,腔內就產生自激振蕩並在後嘴出口形成脈沖
  6. The conclusions are drawn as following : 1. regularity of fabrication in aluminum matrix composite ring - shaped performs with large dimensions and effects of parameters were investigated, based on the novel crucible movable spray deposition technology and equipment. the optimal parameters are that the diameter of the delivery tube is 3. 8mm, spray gas pressure is 0. 8mpa, spray height is 200mm, and transferring pressure of sic is 0. 5mpa

    通過系統的實驗研究得到如下結論: 1 .基於新型的移坩堝自化控制沉積環坯制備技術及裝置,研究了大尺寸鋁基復合材料環坯的制備規律,討論了沉積工藝參數對沉積坯形成過程的影響,得到了最佳工藝參數:導管直徑d = 3 . 8mm ,霧化氣p = 0 . 8mpa ,高度h = 200mm , sic顆粒輸送壓p送= 0 . 5mpa 。
  7. This dissertation has on the research and design of a micro turbine engine as background and it is for the purpose of comprehending viscous flow behaviors in micro scaled conditions and that in the mini - turbine cascades. a mini wind tunnel is designed and set up which also can be used in other micro flow experiments. on the basis of this mini wind tunnel, three mini flow experiments, including micro jet experiment, micro boundary layer experiment and mini - turbine cascades experiment, have been carried out

    本文以某型微型渦輪氣發機研製為背景,以認識微尺度下粘性狀態及其機理和微渦輪葉柵通道內部特性為目的,設計並搭建了除本實驗外還可供其他學實驗使用的微型風洞,並在該微型風洞基礎上進行了微尺度實驗、微尺度壁面邊界層實驗和微尺度渦輪葉柵實驗。
  8. To investigate effect of plenum chamber total pressure on arcjet thruster operation, numerical simulation of operation under various plenum chamber total pressures was performed on the basis of mechanism analysis on its operation and modeling for chemical non - equilibrium flow and steady state electromagnetic field within it

    摘要為了研究集氣腔總壓對電弧器工作過程的影響,在分析其工作機理的基礎上採用化學非平衡和穩態電磁電磁場模型對不同集氣腔總壓下推器工作過程進行了數值模擬。
  9. It is shown that when the exit area of secondary nozzle and the fuel / oxidizer ratio is fixed, the increase of mass flow rate of secondary flow lead to the decrease of velocity of mixed flow, and increase of total mass flow rate. the synthetical result of these two phenomenon cause the increase of thrust of rocket ejector, but the increasing magnitude is relatively small, indicating that these is no necessary to claim large bypass ratio in rocket ejector design. in the comparison between two configurations, the typical one has better performance, indicating the importance of pressure ratio

    結果表明:在固定二次管出口面積和氧燃比的條件下,二次(引空氣量的增加引起混合氣出口速度的下降和總量的增加,二者綜合作用使發機推增加,但增幅不大,表明在設計發機結構和工作參數時,不必過分追求大的引系數;兩種結構的性能對比分析表明了增壓比對引火箭性能的提高具有重要意義;對引火箭的熱循環分析同樣表明,增壓比對于提高發機性能非常關鍵。
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