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Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket ngines.

机译：用于高级火箭发动机的高导热率NaRloy-Z-金刚石复合燃烧室衬里的制作。

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作者
Singh, J.;
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年度 2016
页码 1-7
总页数 7
原文格式 PDF
正文语种 eng
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关键词
High thermal conductivity; Combustion; Advanced rocket engines;

机译：高导热性;燃烧;先进的火箭发动机;

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1. Deposit Formation and Heat Transfer for Bioethanol-Fueled Rocket Engine Combustion Chamber Liners [J] . Azuma Nobuyuki, Hiraiwa Tetsuo, Ogawa Daisuke, Journal of propulsion and power . 2019,第3期

机译：生物乙醇燃料火箭发动机燃烧室衬里的沉积物形成和传热
2. Partial Transparency of Advanced Compression Ignition Combustion Chamber Deposits, Its Impact on Combustion Chamber Wall Temperatures and Application to Thermal Barrier Coating Design [J] . Mark Hoffman, Ryan ODonnell, Zoran Filipi SAE International Journal of Engines . 2018,第2期

机译：先进压缩点火燃烧室沉积物的局部透明度，其对燃烧室壁温度的影响及其在热障涂层设计中的应用
3. Life prediction of thermally highly loaded components: modelling the damage process of a rocket combustion chamber hot wall [J] . W. Schwarz, S. Schwub, K. Quering, CEAS Space Journal . 2011,第1a4期

机译：高负载零件的寿命预测：模拟火箭燃烧室热壁的损坏过程
4. Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket Engines [C] . Biliyar N. Bhat, Sandra E. Greene, Jogender Singh AIAA/ASCE/AHS/ASC structures, structural dynamics and materials conference;AIAA SciTech Forum . 2016

机译：用于高级火箭发动机的高导热率NARloy-Z-金刚石复合燃烧室衬套的制造
5. Fabrication and characterization of high thermal conductivity metal matrix composites using graphite fibers: The next-generation thermal management materials. [D] . Mallim, Sravanthi. 2005

机译：使用石墨纤维的高导热金属基复合材料的制备和表征：下一代热管理材料。
6. Thermal Conductivity of Epoxy Resin Composites Filled with Combustion Synthesized h-BN Particles [O] . Shyan-Lung Chung, Jeng-Shung Lin 2016

机译：燃烧合成的h-BN颗粒填充环氧树脂复合材料的导热系数
7. Fabrication of TBC-armored rocket combustion chambers by EB-PVD methods and TLP assembling [O] . Uwe Schulz, Klaus Fritscher, Manfred Peters, 2005

机译：通过EB-PVD方法和TLP组装制备TBC铠装火箭燃烧室
8. Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket Engines. [R] . Bhat, B. N., Greene, S. E., Singh, J. 2016

机译：用于先进火箭发动机的高导热率NaRloy-Z-金刚石复合燃烧室内衬的制作。

Fabrication of High Thermal Conductivity NARloy-Z-Diamond Composite Combustion Chamber Liner for Advanced Rocket ngines.

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