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- fuel burn rate 燃料燃烧速率
- It seems that matter is lost when fuels burn. 似乎燃料燃烧时物质就消失了。
- Figure 8 -- Burn rate as function of O/F ratio. 图8 -烧伤率为功能的 O / 空燃比。
- Iron oxide may be utilized in achieving propellants of ultrahigh burn rate. 氧化铁可用以制出超高燃速的推进剂。
- Which fuel burns most efficiently? 哪种燃料燃烧效果最佳?
- The thinner of the center electorode,the easier to ignate.It not only makes the ignation more rapid and stable,but aslo makes the fuel burn thorouthly and effcient. 中心电极越细火核越大，点火越迅速、稳定，加速性越强，而且燃烧更充分，更节省燃料
- The hi-tech bubble burst in 2000 was attributed to the high burn rate incurred by IT upstarts. 2000年所出现的高科技泡沫爆破是因为某些资讯科技新贵在公司成立时投资损耗过高。
- While travelling along the conveyor chain, the fuel burns. 燃料在沿着传送线输送时，要燃烧。
- While travelling along the conveyor chain,the fuel burns. 燃料在沿着传送线输送时发生燃烧。
- All burn rate suppressants make the grain more difficult to ignite, necessitating an enhanced pyrotechnic or pyrogen ignition system. 所有烧伤率suppressants ，使粮食更难以点燃，有必要加强烟火材料，或热原点火系统。
- How quickly a fuel burns depends on how well it is mixed with oxygen or air. 燃料如何迅速地燃烧，取决于燃料和氧或空气的混合程度。
- Lampblack (carbon) may slightly increase the burn rate of most propellants through increased heat transfer from the combustion flame to the propellant surface. 油烟（碳）可能略有增加，烧伤率最推进剂，通过增加传热从燃烧火焰向推进剂表面。
- The effects of TMOs and their mixtures on the burning rate and the pressure exponent of the aluminum magnesium fuel rich propellant for unchoked ducted rocket are investigated. 研究了过渡金属氧化物(TMO)及其复配物对非壅塞固体火箭冲压发动机铝镁贫氧推进剂燃烧特性的影响。
- The fuel rich propellant used for the unchoked ram rocket should has high burning rate exponent, appropriate burning rate, low flammability limit and steady combustion properties. 分析结果表明：非壅塞式固体火箭冲压发动机要求贫氧推进剂具有高的燃速压强指数、低的可燃极限和足够好的燃烧稳定性。
- Interstate 91 was shut for hours as more than 10,000 gallons of fuel burned. 91州际公路关闭了数小时，10,000多加仑燃油焚烧殆尽。
- Each tonne of fuel burned also produces 3.2 tonnes of carbon dioxide. 燃烧一公吨燃料要产生3.;2公吨二氧化碳。
- Unfortunately, modifying the burn rate by this means is quite restrictive, as the performance of the propellant, as well as mechanical properties, are also greatly affected by the O/F ratio. 不幸的是，修改烧伤率由这意味着相当的限制，作为表现的推进剂，以及力学性能，也大大受影响的O /空燃比。
- Anderson G W. A Burning Rate Model for Charring Materials[Z]. Gaitherburg:1997. 未定义类型作者.;题名(正体;实词首字母大写)[Z]
- The closed-bomb tests manifest that the apparent burn rates of damaged NEPE propellants vary considerably. 密闭爆发器试验显示,损伤对燃烧稳定有明显影响。
- Winglet designs to act fuel burn 翼梢小翼设计将减少
