{"currentpage":1,"firstResult":0,"maxresult":10,"pagecode":5,"pageindex":{"endPagecode":5,"startPagecode":1},"records":[{"abstractinfo":"为适应未来<span style=\"color:red\">超声速</span><span style=\"color:red\">巡航</span>飞机动力系统的要求,作为一种可能的解决方案,本文对于一类来流为轴向<span style=\"color:red\">超声速</span>、出口为相对亚<span style=\"color:red\">声速</span>的高压比新概念风扇开展了研究,主要采用三维定常粘性数值方法对转子通道内部激波结构进行了初步探讨,根据流场分布构造了转子三维激波结构,为此类风扇气动设计提供了一定的依据.","authors":[{"authorName":"项林","id":"4e2629d8-1606-4bb3-ac09-03d5d11675ab","originalAuthorName":"项林"},{"authorName":"季路成","id":"fd431d6e-0b69-4cce-ab5b-6a2f1d772a81","originalAuthorName":"季路成"},{"authorName":"赵晓路","id":"43684d94-e804-4d07-8a5e-ab504ad6af0b","originalAuthorName":"赵晓路"},{"authorName":"周盛","id":"2afb8c0f-5b9f-4e4b-be72-3ddc805f1aaf","originalAuthorName":"周盛"}],"doi":"","fpage":"699","id":"cbedfc10-9aeb-490e-be3f-92ebc708ae02","issue":"6","journal":{"abbrevTitle":"GCRWLXB","coverImgSrc":"journal/img/cover/GCRWLXB.jpg","id":"32","issnPpub":"0253-231X","publisherId":"GCRWLXB","title":"工程热物理学报   "},"keywords":[{"id":"ddeae032-1ade-4adb-81aa-be82f852f026","keyword":"激波结构","originalKeyword":"激波结构"},{"id":"d0f9a3d6-f5e4-4608-b3ec-39e43c384d3f","keyword":"<span style=\"color:red\">超声速</span>风扇","originalKeyword":"超声速风扇"},{"id":"ec941e95-3030-4354-a7d3-89ddab7d71a6","keyword":"<span style=\"color:red\">超声速</span><span style=\"color:red\">巡航</span>","originalKeyword":"超声速巡航"}],"language":"zh","publisherId":"gcrwlxb200206012","title":"一类高压比新概念风扇转子激波结构探索","volume":"23","year":"2002"},{"abstractinfo":"针对<span style=\"color:red\">超声速</span>特征,建立了适合<span style=\"color:red\">超声速</span>燃烧的扩散火焰面模型.针对某碳氢燃料<span style=\"color:red\">超声速</span>双燃烧室结构,采用k-ωSST湍流模型、扩散火焰面模型和乙烯(C2H4)的31组分128步化学反应机理对<span style=\"color:red\">超声速</span>湍流燃烧流场进行了数值模拟.将计算结果与实验数据进行对比,二者吻合良好,在此基础上,分析了各主要参数的分布规律,结果表明火焰面模型完全适用于<span style=\"color:red\">超声速</span>问题的求解.","authors":[{"authorName":"牛东圣","id":"deb40676-7984-4c37-9717-9648b44f5f0a","originalAuthorName":"牛东圣"},{"authorName":"侯凌云","id":"447d115a-d341-46f6-a12d-32304bd4df6a","originalAuthorName":"侯凌云"}],"doi":"","fpage":"1986","id":"6a53de86-55eb-484e-8d82-7839c6866d44","issue":"10","journal":{"abbrevTitle":"GCRWLXB","coverImgSrc":"journal/img/cover/GCRWLXB.jpg","id":"32","issnPpub":"0253-231X","publisherId":"GCRWLXB","title":"工程热物理学报   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style=\"color:red\">超声速</span>燃烧流场结构、点火与火焰传播特性的影响.","authors":[{"authorName":"孙英英","id":"fb0e322a-0c94-4e7d-a6a8-341908df3266","originalAuthorName":"孙英英"},{"authorName":"韩肇元","id":"cbbd20e6-53f9-4174-83ec-f72bcac063c0","originalAuthorName":"韩肇元"},{"authorName":"司徒明","id":"b7b7c8e4-2377-4b46-9743-4ce1c70c20b1","originalAuthorName":"司徒明"},{"authorName":"琚诒光","id":"36e560fd-2dab-4ac3-814c-eca3ee6140b8","originalAuthorName":"琚诒光"}],"doi":"","fpage":"776","id":"f5957fab-8b8e-4b6b-910d-222b2dddc727","issue":"6","journal":{"abbrevTitle":"GCRWLXB","coverImgSrc":"journal/img/cover/GCRWLXB.jpg","id":"32","issnPpub":"0253-231X","publisherId":"GCRWLXB","title":"工程热物理学报   "},"keywords":[{"id":"3eed2707-547e-4449-80b1-03c0e38db1ac","keyword":"碳氢燃料","originalKeyword":"碳氢燃料"},{"id":"55cc0b06-a914-4416-980b-2cdf48f15bd1","keyword":"点火","originalKeyword":"点火"},{"id":"72589033-2219-49c6-8298-6251f9fb43fe","keyword":"<span style=\"color:red\">超声速</span>燃烧","originalKeyword":"超声速燃烧"}],"language":"zh","publisherId":"gcrwlxb200206035","title":"<span style=\"color:red\">超声速</span>预混可燃气流的点火与燃烧","volume":"23","year":"2002"},{"abstractinfo":"借鉴<span style=\"color:red\">超声速</span>喷管和传统涡轮结构与特性,设计了<span style=\"color:red\">超声速</span>膨胀器.对其内部三维流场的数值研究结果表明,<span style=\"color:red\">超声速</span>膨胀器能够实现气流膨胀加速,膨胀波的出现导致静压沿节距方向分布不均,流道出口附面层分离、回流、低能流体与主流掺混以及激波附面层相互作用是能量损失的主要来源.","authors":[{"authorName":"钟兢军","id":"875133b1-ee0a-4669-b5bd-a1e99ec3fd4e","originalAuthorName":"钟兢军"},{"authorName":"黄振宇","id":"eb32a1a5-7efb-4d5f-b333-2fe26328600f","originalAuthorName":"黄振宇"},{"authorName":"杨凌","id":"8d6452c9-3578-4f65-9496-ce991688ef3c","originalAuthorName":"杨凌"},{"authorName":"韩吉昂","id":"acec757b-8a68-4cd1-bb14-1db0108d5fac","originalAuthorName":"韩吉昂"}],"doi":"","fpage":"60","id":"7873ee9a-f2bb-4325-856c-6046c222a43a","issue":"1","journal":{"abbrevTitle":"GCRWLXB","coverImgSrc":"journal/img/cover/GCRWLXB.jpg","id":"32","issnPpub":"0253-231X","publisherId":"GCRWLXB","title":"工程热物理学报   "},"keywords":[{"id":"95c7b6f8-8091-4729-9287-37705b6b1fbd","keyword":"<span style=\"color:red\">超声速</span>膨胀器","originalKeyword":"超声速膨胀器"},{"id":"e1abff07-3956-4365-9334-a312581073b6","keyword":"膨胀波","originalKeyword":"膨胀波"},{"id":"05cfb0c6-a1ad-40f2-964b-929fcde264fb","keyword":"三维流场","originalKeyword":"三维流场"},{"id":"4e4d4fdd-85d7-4ab5-b048-b9801ca24bbd","keyword":"数值研究","originalKeyword":"数值研究"}],"language":"zh","publisherId":"gcrwlxb201501013","title":"<span style=\"color:red\">超声速</span>膨胀器设计及其内部流动研究","volume":"36","year":"2015"},{"abstractinfo":"简要介绍了高<span style=\"color:red\">超声速</span>飞行器控制面的气动热环境特点,在此基础上,从热管理的角度对各种类型的热防护方案分别进行分析,论证了高<span style=\"color:red\">超声速</span>飞行器控制面采用热结构方案的合理性;并对高<span style=\"color:red\">超声速</span>飞行器控制面热结构方案的特点和进展、改进热结构的途径进行了综述和分析.","authors":[{"authorName":"王立研","id":"b8b8bae2-1be0-4b40-90d3-d0165b543a46","originalAuthorName":"王立研"},{"authorName":"王菁华","id":"168ad6d9-c4b8-4414-b093-91b417a5e32f","originalAuthorName":"王菁华"},{"authorName":"李军","id":"beee5e58-422b-4a04-b3d4-ebffe08ac8b5","originalAuthorName":"李军"},{"authorName":"杨炳尉","id":"a9bfce73-5ace-4754-895b-dbfb0ce97f7d","originalAuthorName":"杨炳尉"},{"authorName":"陈浩","id":"f8ab1a03-9ee5-467b-b587-38176282b192","originalAuthorName":"陈浩"}],"doi":"10.3969/j.issn.1007-2330.2016.01.002","fpage":"7","id":"ea1f33ea-cc66-4e68-acfa-39f6c5ea3c32","issue":"1","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"b400197a-b0e2-453f-b1e1-d603585b11d9","keyword":"控制面","originalKeyword":"控制面"},{"id":"54c9fe65-74f6-42e7-9da7-5b3bec40dc28","keyword":"气动热","originalKeyword":"气动热"},{"id":"4f6dbcd6-4807-4c24-9a42-42603934c869","keyword":"热管理","originalKeyword":"热管理"},{"id":"f668cf9b-4969-4e32-9377-7dcc4912c2c4","keyword":"热防护","originalKeyword":"热防护"},{"id":"ecadc55a-1a26-4a5c-b797-538059923014","keyword":"热结构","originalKeyword":"热结构"}],"language":"zh","publisherId":"yhclgy201601002","title":"高<span style=\"color:red\">超声速</span>飞行器控制面热防护技术跟踪研究","volume":"46","year":"2016"},{"abstractinfo":"简要叙述了临近空间的定义及临近空间的飞行器类型,回顾了美国临近空间高<span style=\"color:red\">超声速</span>飞行器的发展历程,主要介绍猎鹰计划的研究目标及军事应用,重点介绍猎鹰计划中高<span style=\"color:red\">超声速</span>飞行器防热材料的发展.","authors":[{"authorName":"张友华","id":"378e82c6-c576-44a2-ba89-891b2a28874a","originalAuthorName":"张友华"},{"authorName":"陈连忠","id":"e373006e-b8a4-4edf-a9c9-3055dd4a8f30","originalAuthorName":"陈连忠"},{"authorName":"张敏莉","id":"525e5ac5-f9a7-45a2-8c7a-4d6eb36c0965","originalAuthorName":"张敏莉"}],"doi":"","fpage":"12","id":"6e3837ae-1258-43ff-9915-e7cdb4fc0a95","issue":"6","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"73783282-fcd5-4d8a-a123-0a26c4a2c36c","keyword":"临近空间","originalKeyword":"临近空间"},{"id":"df85a4c4-146e-4d7d-b2cf-471e82ffd812","keyword":"高<span style=\"color:red\">超声速</span>飞行器","originalKeyword":"高超声速飞行器"},{"id":"2b725a8b-edb4-4db8-b2ea-c03a9412b950","keyword":"防热材料","originalKeyword":"防热材料"},{"id":"9ff31222-b966-4096-ae3d-d9ca8712c857","keyword":"猎鹰计划","originalKeyword":"猎鹰计划"}],"language":"zh","publisherId":"yhclgy201206002","title":"临近空间高<span style=\"color:red\">超声速</span>飞行器防热材料的发展","volume":"42","year":"2012"},{"abstractinfo":"描述了<span style=\"color:red\">超声速</span>导弹弹体的热环境,高温树脂基复合材料基体候选树脂,重点介绍了双马来酰亚胺、聚酰亚胺树脂和氰酸酯的性能及最新进展,最后描述了高温树脂基复合材料在<span style=\"color:red\">超声速</span>导弹弹体上的应用研究.","authors":[{"authorName":"刘萝威","id":"48900caa-eb6b-4391-b35e-e20258dfaf06","originalAuthorName":"刘萝威"},{"authorName":"曹运红","id":"d5c990f9-3174-4ca4-958a-a44f2029cc25","originalAuthorName":"曹运红"}],"doi":"10.3969/j.issn.1007-2330.2002.05.004","fpage":"15","id":"c5ad77b7-e0c4-4040-9479-d9c45bb5d7e7","issue":"5","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"92120b7e-cc7c-4981-b256-9d7f90d2a810","keyword":"弹体","originalKeyword":"弹体"},{"id":"225f1f88-c813-4628-90a7-31dca4110769","keyword":"树脂基复合材料","originalKeyword":"树脂基复合材料"},{"id":"d09b3b95-ff59-4347-bcb9-af1dfe23c98c","keyword":"<span style=\"color:red\">超声速</span>导弹","originalKeyword":"超声速导弹"},{"id":"5cab21c7-e7da-4da3-a219-5291fcf2684d","keyword":"双马来酰亚胺","originalKeyword":"双马来酰亚胺"},{"id":"03054bb4-6e26-4a99-8149-4f5562cfcdbe","keyword":"聚酰亚胺树脂","originalKeyword":"聚酰亚胺树脂"},{"id":"fe542a20-ec17-4982-b66f-6266eca35c8e","keyword":"氰酸酯","originalKeyword":"氰酸酯"}],"language":"zh","publisherId":"yhclgy200205004","title":"高温树脂基复合材料在<span style=\"color:red\">超声速</span>导弹弹体上的应用","volume":"32","year":"2002"},{"abstractinfo":"综述了以刚性陶瓷隔热瓦、陶瓷纤维隔热毡及轻质烧蚀材料为代表的飞行器隔热材料技术最新研究进展,详细介绍了这些隔热材料的组成、结构和性能特点,总结了这些材料在高<span style=\"color:red\">超声速</span>飞行器上的应用,展望了高<span style=\"color:red\">超声速</span>飞行器隔热材料的未来发展.","authors":[{"authorName":"李俊宁","id":"1480baad-fed6-40b8-bf15-141ac3c3aa3f","originalAuthorName":"李俊宁"},{"authorName":"胡子君","id":"d5b224b3-49f0-41c6-86e8-56e5f406ae02","originalAuthorName":"胡子君"},{"authorName":"孙陈诚","id":"45913d86-336e-44de-b7c4-55d09f9e521e","originalAuthorName":"孙陈诚"},{"authorName":"吴文军","id":"70189021-cfe5-4dee-86f9-7eb66e551389","originalAuthorName":"吴文军"},{"authorName":"张宏波","id":"0d276bc2-b1ae-453c-b698-13e583022cd3","originalAuthorName":"张宏波"}],"doi":"10.3969/j.issn.1007-2330.2011.06.003","fpage":"10","id":"7d49a183-b3b4-4e4c-8876-ccd3c972ce36","issue":"6","journal":{"abbrevTitle":"YHCLGY","coverImgSrc":"journal/img/cover/YHCLGY.jpg","id":"77","issnPpub":"1007-2330","publisherId":"YHCLGY","title":"宇航材料工艺   "},"keywords":[{"id":"5245d155-adf0-43ac-9926-b3623e9b68d9","keyword":"高<span style=\"color:red\">超声速</span>飞行器","originalKeyword":"高超声速飞行器"},{"id":"0d7de1a9-95e0-418c-b611-3e1d3b7200e0","keyword":"隔热材料","originalKeyword":"隔热材料"},{"id":"d5a7dca9-4da0-4a71-b98d-7e302d28203a","keyword":"陶瓷瓦","originalKeyword":"陶瓷瓦"},{"id":"bd28c244-57ce-4323-bc4f-8c13dcc2f8ad","keyword":"隔热毡","originalKeyword":"隔热毡"},{"id":"c77c20a7-1a4d-46af-a540-d18e8d0374dd","keyword":"烧蚀","originalKeyword":"烧蚀"}],"language":"zh","publisherId":"yhclgy201106003","title":"高<span style=\"color:red\">超声速</span>飞行器隔热材料技术研究进展","volume":"41","year":"2011"},{"abstractinfo":"建立飞行器的热走廊物理模型和求解方法对于设计飞行器防热结构、确定飞行轨道和优化气动外形等均有重要的工程应用价值,本文对X43高<span style=\"color:red\">超声速</span>飞行器的飞行热走廊的物理含义进行了分析,初步建立了飞行热走廊的物理模型,给出了该物理模型下飞行热走廊的控制方程和求解方法,通过对X43高<span style=\"color:red\">超声速</span>飞行器典型位置的飞行热走廊的计算,研究了高<span style=\"color:red\">超声速</span>飞行器的热走廊规律和特征,研究了防热材料的性能对飞行走廊的限制,明确了防热材料的关键防热参数,通过研究发现: (1)防热材料的发射系数越大,其对应的热走廊越宽阔,飞行轨道的选择余地也越大; (2)不同位置、不同流态对应的热走廊边界不同,推迟转捩发生可以增加热走廊区域,有利于防热.","authors":[{"authorName":"金玲","id":"5eab2fec-c0d2-45ca-bf38-f45767e7f773","originalAuthorName":"金玲"},{"authorName":"王安龄","id":"2c665e21-0894-401f-8b6b-35dd8e6291c0","originalAuthorName":"王安龄"},{"authorName":"桂业伟","id":"891c635a-8fcf-41a7-a5c7-ace618ad5030","originalAuthorName":"桂业伟"},{"authorName":"耿湘人","id":"ecfe3611-0534-4921-a5bf-1ced606f653e","originalAuthorName":"耿湘人"},{"authorName":"唐伟","id":"6de65087-53dd-4fcf-a397-88373e83c011","originalAuthorName":"唐伟"}],"doi":"","fpage":"325","id":"927a8a1e-8aa9-4039-8608-2505ad1207c4","issue":"2","journal":{"abbrevTitle":"GCRWLXB","coverImgSrc":"journal/img/cover/GCRWLXB.jpg","id":"32","issnPpub":"0253-231X","publisherId":"GCRWLXB","title":"工程热物理学报   "},"keywords":[{"id":"d2efe4ab-3ff9-4c06-917e-30254414a1bd","keyword":"气动热","originalKeyword":"气动热"},{"id":"816a1e39-a8a3-4375-b990-a8e84dff6806","keyword":"热防护","originalKeyword":"热防护"},{"id":"17aca992-3dff-4c55-898e-c52021350157","keyword":"热走廊","originalKeyword":"热走廊"}],"language":"zh","publisherId":"gcrwlxb200702046","title":"X43高<span style=\"color:red\">超声速</span>飞行器的飞行热走廊研究","volume":"28","year":"2007"},{"abstractinfo":"本文使用了直接模拟（DNS）程序计算了三维<span style=\"color:red\">超声速</span>湍流射流火焰。首先介绍了本程序使用到的计算方法，包括热物性参数和输运参数的计算、反应机理、边界条件、离散方法。然后，本文使用该方法计算了马赫数为12的三维<span style=\"color:red\">超声速</span>H2-AIR湍流射流火焰，描述了火焰的整体结构。最后，本文对火焰底部的稳燃的机理～自燃进行了分析和论证。","authors":[{"authorName":"卢树强","id":"7edbd588-3162-40e2-a342-5271fe52d254","originalAuthorName":"卢树强"},{"authorName":"李德波","id":"ee25ef50-0c17-435d-a21c-6566db1139ec","originalAuthorName":"李德波"},{"authorName":"易富兴","id":"ebd18bc4-6a96-4d69-80c3-31db2d500a50","originalAuthorName":"易富兴"},{"authorName":"罗坤","id":"c8b7ff59-fe56-439c-90c7-d314f3b54f95","originalAuthorName":"罗坤"},{"authorName":"樊建人","id":"18c3c026-6d86-4d9e-9168-735fb85e16e9","originalAuthorName":"樊建人"}],"doi":"","fpage":"326","id":"1c13e8b5-78e0-46d1-a485-2629d5e2dc68","issue":"2","journal":{"abbrevTitle":"GCRWLXB","coverImgSrc":"journal/img/cover/GCRWLXB.jpg","id":"32","issnPpub":"0253-231X","publisherId":"GCRWLXB","title":"工程热物理学报   "},"keywords":[{"id":"3a8de21b-423d-45a9-95d5-e32a464925c4","keyword":"DNS","originalKeyword":"DNS"},{"id":"e3e4cf50-aafa-4bbd-8841-7e9ae2fdca49","keyword":"<span style=\"color:red\">超声速</span>","originalKeyword":"超声速"},{"id":"a831e9d4-a283-49ff-83d5-d5d9466fd64a","keyword":"射流火焰","originalKeyword":"射流火焰"},{"id":"acdcd1f2-e69c-4bf6-99c6-d33ac61ae8c9","keyword":"自燃","originalKeyword":"自燃"}],"language":"zh","publisherId":"gcrwlxb201202039","title":"三维<span style=\"color:red\">超声速</span>射流火焰的直接模拟研究","volume":"33","year":"2012"}],"totalpage":304,"totalrecord":3034}