Notice: error_log(): write of 356 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Notice: error_log(): write of 94 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Notice: error_log(): write of 107 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Notice: error_log(): write of 47 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Notice: error_log(): write of 67 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Notice: error_log(): write of 143 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Warning: file_put_contents(/www/wwwroot/seo-dashuju-wenxue/cache/words/v/2b971e8c58cba5e8ae9a168c959cc49b.html): failed to open stream: No space left on device in /www/wwwroot/seo-dashuju-wenxue/main/table/Router.php on line 608
Notice: error_log(): write of 285 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Notice: error_log(): write of 106 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199
Notice: error_log(): write of 114 bytes failed with errno=28 No space left on device in /www/wwwroot/seo-dashuju-wenxue/code/logginfo/SimpleLogger.php on line 199 “GTC”是“Gas Turbine Compressor”的缩写，意思是“燃气轮机压缩机”-机构类英文缩写翻译大全
Gas turbine compressor high supercharged engine of low compression ratio 燃气轮机压缩机(GTC)燃气涡轮压缩机低压缩比高增压发动机
Quantitative HAZOP analysis for gas turbine compressor unit based on fuzzy information fusion theory 基于模糊信息融合的燃压机组定量HAZOP分析
Gas turbine compressor double-extraction non-condensing turbine 双抽气背压式汽轮机
The quenching process of gas turbine compressor disk was simulated to study the stress field by finite element method. 利用有限元法研究了某重型燃机压气机盘在淬火过程中的应力场分布。
From this point the work establishes aerodynamic optimization design system that is applicable to heavy-duty gas turbine compressor by introducing optimization theory to heavy-duty gas turbine compressor blade design. 本文的工作就是从这一方面着手，将优化理论引入到地面重型燃气轮机压气机叶型设计中，建立可用于地面重型燃气轮机压气机的二维气动优化设计体系。