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  • Fluidic Nozzle to Improve Transonic Pitch and Thrust Performance of Hypersonic Vehicle 发布日期:2013-07-04 13:55:13 好评:600 浏览次数:9359

    [唯一标识符]:CDSTIC.AIAA 2005-3501[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:Fluidic Nozzle to Improve Transonic Pitch and Thrust Performance of Hypersonic Vehicle[作者]:Eric J Gamble[出版单位]:美国航空航天局[文摘]:1American Institute of Aeronautics and AstronauticsFLUIDIC NOZZL...[阅读全文]

  • A Computational Study of a Dual Throat Fluidic Thrust Vectoring Nozzle Concept 发布日期:2013-07-04 13:55:13 好评:849 浏览次数:9578

    [唯一标识符]:CDSTIC.AIAA 2005-3502[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:A Computational Study of a Dual Throat Fluidic Thrust Vectoring Nozzle Concept[作者]:Karen A Deere[出版单位]:美国航空航天局[文摘]:American Institute of Aeronautics and Astronautics1A Computational Study...[阅读全文]

  • Control of the attitude and position of a synchronous satellite by continuous radial thrust./用持续径向动力控制同步卫星的姿态与方位 发布日期:2013-07-04 13:55:13 好评:985 浏览次数:6273

    [唯一标识符]:CDSTIC.AIAA.1963-0008A[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:Control of the attitude and position of a synchronous satellite by continuous radial thrust./用持续径向动力控制同步卫星的姿态与方位[作者]:Toms; R. S. H.; Kalensher; B. E.[出版单位]:美国航空航天局[关键词]:Satellite attitud...[阅读全文]

  • The hall current plasma accelerator/霍尔感应电流等离子体加速器 发布日期:2013-07-04 13:55:13 好评:718 浏览次数:7854

    [唯一标识符]:CDSTIC.AIAA.1963-0011[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:The hall current plasma accelerator/霍尔感应电流等离子体加速器[作者]:Cann; G. L.[出版单位]:美国航空航天局[关键词]:PLasma physics, Ion accelerators, Electric propulsion[出版时间]:1963[出版年份]:1963[报告号]:AIAA63-0011[会议名称]:AIA...[阅读全文]

  • Analytical performance of a pinch plasma accelerator/引缩等离子体加速器的分析性能 发布日期:2013-07-04 13:55:13 好评:730 浏览次数:6232

    [唯一标识符]:CDSTIC.AIAA.1963-0014B[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:Analytical performance of a pinch plasma accelerator/引缩等离子体加速器的分析性能[作者]:Mcilroy; W.[出版单位]:美国航空航天局[关键词]:Plasma physics, Magnetic pinch, Particle accelerators[出版时间]:1963[出版年份]:1963[报告号]:Co...[阅读全文]

  • Experimental Study of a Dual-Throat Fluidic Thrust-Vectoring Nozzle Concept 发布日期:2013-07-04 13:55:13 好评:638 浏览次数:8827

    [唯一标识符]:CDSTIC.AIAA 2005-3503[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:Experimental Study of a Dual-Throat Fluidic Thrust-Vectoring Nozzle Concept[作者]:Jeffrey D Flamm[出版单位]:美国航空航天局[文摘]:American Institute of Aeronautics and Astronautics1Experimental Study of ...[阅读全文]

  • Subsonic and Transonic Jet Control with Cross-Wire 发布日期:2013-07-04 13:55:13 好评:753 浏览次数:6712

    [唯一标识符]:CDSTIC.AIAA 2005-3504[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:Subsonic and Transonic Jet Control with Cross-Wire[作者]:Ethirajan Rathakrishnan[出版单位]:美国航空航天局[文摘]:Subsonic and Transonic Jet Control with Cross-WireP. Lovaraju and E. RathakrishnanyDepar...[阅读全文]

  • Surface ionization microscope/表面电离显微镜 发布日期:2013-07-04 13:55:13 好评:720 浏览次数:8994

    [唯一标识符]:CDSTIC.AIAA.1963-0018[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:Surface ionization microscope/表面电离显微镜[作者]:Marchant; A. B.[出版单位]:美国航空航天局[关键词]:Cesium, Ionization, Microscope[出版时间]:1963[出版年份]:1963[报告号]:AIAA63-0018[会议名称]:AIAA Electric Propulsion Conferenc...[阅读全文]

  • Energy addition and loss mechanisms in the thermal arc jet engine/在热电弧喷气发动机中能的追加与损失机理 发布日期:2013-07-04 13:55:13 好评:836 浏览次数:7532

    [唯一标识符]:CDSTIC.AIAA.1963-0022[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:Energy addition and loss mechanisms in the thermal arc jet engine/在热电弧喷气发动机中能的追加与损失机理[作者]:John; R. R.[出版单位]:美国航空航天局[关键词]:Electric propulsion, Plasma jet, Exhaust nozzles, Jet engines[出版时间...[阅读全文]

  • High-frequency supersonic heating of hydrogen for propulsion/推进用氢的高频超音速加热 发布日期:2013-07-04 13:55:13 好评:856 浏览次数:9407

    [唯一标识符]:CDSTIC.AIAA.1963-0026[文献来源]:美国航空航天学会会议(AIAA)[文献类型]:科技会议[标题]:High-frequency supersonic heating of hydrogen for propulsion/推进用氢的高频超音速加热[作者]:Bonneville; J. N.[出版单位]:美国航空航天局[关键词]:Hydrogen, Heating-High frequency, Supersonic flow, Electric propulsion[出...[阅读全文]

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