模擬火箭 的英文怎麼說
中文拼音 [mónǐhuǒjiàn]
模擬火箭
英文
simulated rocket-
Mayer a e h j, stowe r a. experimental study into mixing in a solid fuel ducted rocket combustion chamber [ r ]. aiaa 2000 - 3346
餘勇，陳小前，等.三維實驗固體火箭沖壓發動機燃燒室湍流反應流數值模擬[ j ] .國防科技大學學報， 2002 ， （ 5 ）Ground test equipment training simulation system based on off - ballistic trajectory measure and wireless security system of launch vehicle
運載火箭外測安全系統地面測試設備模擬訓練系統Then, with yankees vice president of player personnel billy connors and pitching prospects phil hughes, jeff karstens, joba chamberlain, christian garcia and jose veras looking on, clemens tossed a simulated session with minor leaguers hector gonzalez and kevin smith acting as batters in the box
之後在洋基球員管理部副總康諾斯和新人投手休斯、卡斯坦、張伯倫、賈西亞和維拉斯環視之下，火箭人跟小聯盟打者岡薩勒斯和史密斯進行了一場模擬賽。The 3 - d complex flowfield of rocket - missile with wings and empennages induced by the interaction between by base jet and the flow around the body has been numerically simulated. the main work is as follows : first, the gordon - mcbride program was developed to make it more friendly and efficient to the users
本文對帶彈翼/尾翼彈箭的三維噴流繞流復雜流場進行了數值模擬，其主要研究內容有：首先，對gordon - mcbride火箭程序作了改進，使改進后的軟體具有了非常友好的人機交互界面。Study on boiling heat transfer enhancement of forced liquid nitrogen flow in lunate narrow channel
低溫液體火箭發動機循環預冷模擬試驗Then, the navier - stokes equations for 2 - d axisymmetric compressible turbulent flow were constructed and phoenics was used to simulate the 2 - d axisymmetric compressible turbulent flowfield of rocket jet
其次，建立了二維軸對稱可壓縮湍流流動的平均navier - stokes方程，並利用phoenics軟體對二維軸對稱火箭噴流進行了數值模擬。The study of launching dynamics simulation for multiple rocket launcher
多管火箭炮系統發射動力學模擬研究Design of the multiple rocket launcher loading training simulator based on vr
的火箭炮裝填訓練模擬器的設計Fifth, vpm is real - time digital simulation system software of launch vehicle and missile
5 、 vpm是運載火箭和導彈的實時數字模擬軟體系統。Based on the simulation system software, navigation and guidance real - time digital simulation system are developed to simulate the whole real - time flight control and guidance process
本文利用vpm平臺，建立運載火箭迭代制導系統的導航和導引模型，形成模塊化的數字模擬系統。Aiming at the conveying - alcohol pipe system of a certin model gas generator in our school rocket engine field laboratory, this paper does a series of simulation studies using amesim, analyses and summarizes the results of simulations, and at the same time implements some waterhammer experiments, and compares the results with the ones of simulations
本文針對我校火箭發動機試驗外場的某型燃發器試驗酒精供應管道系統，使用amesim進行了一系列的模擬研究，對模擬的結果進行了分析和總結，同時還開展了水擊試驗，並與模擬進行了對比。For the inaugural flight, the rocket, made by the boeing company, will carry a 13, 000 - pound dummy satellite and then crash into the atlantic ocean
在由波音公司研製的該型火箭的初次發射中，其將攜帶1萬三千磅的模擬衛星並將最終墜毀于大西洋中。For studying the performance of solid rocket ramjet under the influence of different flight conditions, it ' s significant to simulate the integrated flow field of inlet and combustor
因此，開展超聲速進氣道/補燃室流場一體化數值模擬研究對于考查飛行狀態對於火箭沖壓發動機性能的直接影響具有重要的現實意義。Through malfunction of the tests of 810 research institute, the combustion performance of the hybrid motor and model about regression rate have been studied in the dissertation. the main aspects are as follows : the performance of the hno3 + n2o4 - htpb hybrid rocket motor were all discussed
本文結合航天科技集團公司810研究所正在研製的ak - 20l / htpb + al組合固液火箭發動機，開展了固液火箭發動機混合燃燒特性的數值模擬工作，在此基礎上給出固體燃料退移速率預示模型及預示結果。Simulation and test of rocket initial disturbance
火箭彈起始擾動的模擬與試驗研究New developments in decision theory, artificial theory and dynamic analysis method are applied to evaluation the possible projects. the main contents in this paper are included as follows : first, has improved an format reasoning method based on multiple attribute utility model and knowledgebase theory ; second, has proposed complex utility model by improving the theory of multiple attribute utility ; third, has presented a kind of weapon intelligent decision support system, based on the complex utility model and developed with com / dcom criterion ; forth, this paper also has build the dynamic simulation model for long - rang multiple tube rocket launcher system, and the tire dynamic model has applied in the rocket launcher system dynamic simulation model ; fifth, through building the rocket - launcher contact model, this paper has analyzed the dynamic forces between the rocket and launcher ; finally, this paper has build the evaluation model of the project about improving existing rocket launcher to the launcher that using canister, and get the conclusion through using the widss. the studies in this paper not only proposed scientific warrant to the choice of projects in this pre - studied national defense task about improving existing rocket launcher to the launcher that using canister, but also can give other studied tasks with decision supported
主要內容包括：在總結決策分析與專家系統規則庫技術的基礎上，提出了融決策分析與專家系統規則庫技術於一體的形式化推理機制，該機制能有效的將定量計算和定性知識融為一體，將規范的決策分析解題過程與專家系統特有的演化推理方法有機結合起來；在多屬性效用理論的基礎上，建立了一般形式的復式效用模型，並實用化了全相關乘式效用模型，提供了較完善的通用建模、分析和解釋功能：引入了com dcom組件技術，開發了基於組件的widss系統，該系統基於形式化推理機制，易於擴展，能夠面向多種決策問題，具有較強的通用性；建立了遠程多管火箭炮全炮動力學模擬模型，將充氣輪胎動力學模型、輪胎和路面的相互作用模型運用於多管火箭炮動力學模擬計算中；利用碰撞接觸理論，對火箭彈在定向器管內的運動受力情況進行了模擬計算；建立了遠程多管火箭炮箱式發射改進方案模型，並利用動力學模擬計算結果在widss系統中進行了方案性能評估。The study of launch vehicle platform align emulation system
運載火箭初始對準模擬系統的研究The simulation and analysis of failure matter in a servo system used in a rocket
運載火箭伺服系統電路故障模式模擬分析The effect of range correction system of long - range rocket adopting sins is analyzed through numerical simulation
通過數值模擬的方法，研究了採用捷聯慣導技術后遠程火箭射程修正效果。It is important to develop experiment techniques to simulate flow field in the study of solid rocket motor with high acceleration
本文以高過載固體火箭發動機研製需求為背景，圍繞高過載發動機內流場的地面模擬試驗技術展開研究。分享友人