concurrent computation中文是什么意思

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中文翻譯
造句

并行計(jì)算

concurrent adj. 1.同時(shí)發(fā)生的，并發(fā)的，并存的，共存的；合作的 ...
computation n. 1.計(jì)算，估算。 2.計(jì)算法。 3.計(jì)算結(jié)果，得數(shù) ...
concurrent adj. 1.同時(shí)發(fā)生的，并發(fā)的，并存的，共存的；合作的。 2.(意見)一致的。 3.【動(dòng)物；動(dòng)物學(xué)】趨合的；【數(shù)學(xué)】共點(diǎn)的；【機(jī)械工程】并流的。 4.(權(quán)力等)由兩個(gè)負(fù)責(zé)當(dāng)局共同行使的，有相等裁定權(quán)的。 concurrent insurance (policy) (對(duì)于一投保物的)共同保險(xiǎn)(合同)。 concurrent post 兼職。 concurrent sentence (適用于多個(gè)被告的)共同判決。 n. 1.并發(fā)事件；共存[共有]物；并在原因。 2.競(jìng)爭(zhēng)者。 3.【數(shù)學(xué)】共點(diǎn)。 adv. -ly (hold a post concurrently 兼任)。
concurrent with 和...同時(shí)
computation n. 1.計(jì)算，估算。 2.計(jì)算法。 3.計(jì)算結(jié)果，得數(shù)。
bus, concurrent 并行總線
concurrent access 并行存取, 并行訪問; 并行訪向
concurrent actions 共同訴訟
concurrent activities 并行動(dòng)作; 并行活動(dòng)
concurrent appointment 同時(shí)委任
concurrent arbitration 聯(lián)合仲裁
concurrent assignment 并行賦值
concurrent audit 事中審計(jì)
concurrent authority 同等權(quán)力
concurrent axes 交叉軸; 相交軸
concurrent axis 相交軸
concurrent boiler 順流鍋爐; 直流鍋爐
concurrent bus 并行總線
concurrent causes 并存原因; 并行原因
concurrent centrifuge 并嶺心機(jī); 順流式離心機(jī); 無逆流離心機(jī)
concurrent characteristic 并發(fā)特性
concurrent communication 并行通信
concurrent competence 共同權(quán)限; 平行職權(quán)
concurrent computer 并行操作計(jì)算機(jī); 并行計(jì)算機(jī)
concurrent concession 同時(shí)讓步

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例句與用法

Significant advances in parallel algorithms and architectures have demonstrated the potential for applying concurrent computation techniques to a wide variety of problems
廣泛開拓并行應(yīng)用體系是當(dāng)務(wù)之急。伴隨著國(guó)際互連網(wǎng)的發(fā)展，人們對(duì)多媒體信息的需求與日俱增。
Abstract : a new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
文摘:探討了一種新的設(shè)計(jì)指標(biāo)最優(yōu)分配方法- -協(xié)同分配法,用于處理飛機(jī)頂層設(shè)計(jì)中的大規(guī)模設(shè)計(jì)指標(biāo)最優(yōu)分配問題.分析了飛機(jī)頂層設(shè)計(jì)中的設(shè)計(jì)指標(biāo)最優(yōu)分配特征,據(jù)此給出了協(xié)同法的原理并建立了數(shù)學(xué)模型.協(xié)同法按設(shè)計(jì)指標(biāo)分配關(guān)系將最優(yōu)分配問題分解為主系統(tǒng)優(yōu)化和子系統(tǒng)優(yōu)化,主優(yōu)化對(duì)子系統(tǒng)設(shè)計(jì)指標(biāo)進(jìn)行最優(yōu)分配,子優(yōu)化以最小化分配設(shè)計(jì)指標(biāo)值與期望設(shè)計(jì)指標(biāo)值之間的差異為目標(biāo),進(jìn)行子系統(tǒng)最優(yōu)設(shè)計(jì),或?qū)Φ讓釉?如飛機(jī)翼梁、翼肋和翼盒等)進(jìn)行設(shè)計(jì)指標(biāo)最優(yōu)分配,并把最優(yōu)解信息反饋給主優(yōu)化.主優(yōu)化通過子優(yōu)化最優(yōu)解信息構(gòu)成的一致性約束協(xié)調(diào)分配量,提高系統(tǒng)整體性能,并重新給出分配方案.主系統(tǒng)與子系統(tǒng)反復(fù)協(xié)調(diào),直到得到設(shè)計(jì)指標(biāo)最優(yōu)分配方案.兩層可靠度指標(biāo)分配算例初步驗(yàn)證了本文方法的正確性與可行性,三層可靠度指標(biāo)分配算例證明了本文方法的有效性.最后,以重量指標(biāo)分配為例,簡(jiǎn)要敘述了針對(duì)飛機(jī)頂層設(shè)計(jì)中設(shè)計(jì)指標(biāo)協(xié)同分配的數(shù)學(xué)模型和求解思路
A new method , collaborative allocation ( ca ) , is proposed to solve the large - scale optimum allocation problem in aircraft conceptual design . according to the characteristics of optimum allocation in aircraft conceptual design . the principle and mathematical model of ca are established . the optimum allocation problem is decomposed into one main optimization problem and several sub - optimization problems . a group of design requirements for subsystems are provided by the main system respectively , and the subsystems execute their own optimizations or further provide the detailed design requirements to the bottom components of aircraft , such as spars , ribs and skins , etc . the subsystems minimize the discrepancy between their own local variables and the corresponding allocated values , and then return the optimization results to main optimization . the main optimization is performed to reallocate the design requirements for improving the integration performance and progressing toward the compatibilities among subsystems . ca provides the general optimum allocation architecture and is easy to be carried out . furthermore , the concurrent computation can also be realized . two examples of optimum reliability allocation are used to describe the implementation procedure of ca for two - level allocation and three - level allocation respectively , and to validate preliminarily its correctness and effectiveness . it is shown that the developed method can be successfully used in optimum allocation of design requirements . then taking weight requirement allocation as example , the mathematical model and solution procedure for collaborative allocation of design requirements in aircraft conceptual design are briefly depicted
探討了一種新的設(shè)計(jì)指標(biāo)最優(yōu)分配方法- -協(xié)同分配法,用于處理飛機(jī)頂層設(shè)計(jì)中的大規(guī)模設(shè)計(jì)指標(biāo)最優(yōu)分配問題.分析了飛機(jī)頂層設(shè)計(jì)中的設(shè)計(jì)指標(biāo)最優(yōu)分配特征,據(jù)此給出了協(xié)同法的原理并建立了數(shù)學(xué)模型.協(xié)同法按設(shè)計(jì)指標(biāo)分配關(guān)系將最優(yōu)分配問題分解為主系統(tǒng)優(yōu)化和子系統(tǒng)優(yōu)化,主優(yōu)化對(duì)子系統(tǒng)設(shè)計(jì)指標(biāo)進(jìn)行最優(yōu)分配,子優(yōu)化以最小化分配設(shè)計(jì)指標(biāo)值與期望設(shè)計(jì)指標(biāo)值之間的差異為目標(biāo),進(jìn)行子系統(tǒng)最優(yōu)設(shè)計(jì),或?qū)Φ讓釉?如飛機(jī)翼梁、翼肋和翼盒等)進(jìn)行設(shè)計(jì)指標(biāo)最優(yōu)分配,并把最優(yōu)解信息反饋給主優(yōu)化.主優(yōu)化通過子優(yōu)化最優(yōu)解信息構(gòu)成的一致性約束協(xié)調(diào)分配量,提高系統(tǒng)整體性能,并重新給出分配方案.主系統(tǒng)與子系統(tǒng)反復(fù)協(xié)調(diào),直到得到設(shè)計(jì)指標(biāo)最優(yōu)分配方案.兩層可靠度指標(biāo)分配算例初步驗(yàn)證了本文方法的正確性與可行性,三層可靠度指標(biāo)分配算例證明了本文方法的有效性.最后,以重量指標(biāo)分配為例,簡(jiǎn)要敘述了針對(duì)飛機(jī)頂層設(shè)計(jì)中設(shè)計(jì)指標(biāo)協(xié)同分配的數(shù)學(xué)模型和求解思路

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