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工作OKRs/25.9-11 OKR.canvas
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{"id":"8359617e1edc48ba","type":"text","text":"状态指标：\n推进OKR的时候也要关注这些事情，它们是完成OKR的保障。\n\n\n效率状态 green","x":-76,"y":-306,"width":456,"height":347},
{"id":"a4eaccbbfadaaf17","type":"text","text":"# 目标：\n多体模块完善 线性化模块开发\n### 每周盘点一下它们\n\n\n关键结果：多体动力学建模原理、建模方法、线性化原理掌握 （9/10）\n\n关键结果：风机多体动力学文献调研情况完成 （5.5/10）\n关键结果：目标工况测试、稳态工况对比 （5/10）","x":-76,"y":-803,"width":456,"height":457},
{"id":"d2c5e076ba6cf7d7","type":"text","text":"# 推进计划\n未来四周计划推进的重要事情\n\n文献调研启动\n\n建模重新推导\n\n\n","x":-600,"y":-306,"width":456,"height":347},
{"id":"82708a439812fdc7","type":"text","text":"# 10月已完成\n\n","x":-220,"y":134,"width":440,"height":560},
{"id":"82708a439812fdc7","type":"text","text":"# 10月已完成\n\n- 编写输出量\n\t- 方法测试 done\n\t- 批量输出编写 done","x":-220,"y":134,"width":440,"height":560},
{"id":"505acb3e6b119076","type":"text","text":"# 9月已完成\n\nP1 湍流 气动 多体 控制联调 done\n- 5mw 通了\n\t- 纯叶片变形\n\t- 纯塔架变形\n\t- 叶片+塔架变形 \n\nP1 bladed对比--稳态运行载荷，产出报告\n- 气动新版本稳态跑通 done\n- 多体模块输出方法更新\n\t- 增加输出结构体\n\t- 新增输出宏，自动编写变量头和输出\n\t- 输出位置从ed_calcoutput拆分\n- 稳态变形量对比\n- 所有输出量梳理，对比","x":-700,"y":134,"width":440,"height":560},
{"id":"30cb7486dc4e224c","type":"text","text":"# 11月已完成\n\n\n\n","x":260,"y":134,"width":440,"height":560},
{"id":"c18d25521d773705","type":"text","text":"# 计划\n这周要做的3~5件重要的事情，这些事情能有效推进实现OKR。\n\nP1 必须做。P2 应该做\n\n\nP2 柔性部件 叶片、塔架变形算法 主线\n- 变形体动力学 简略看看ing\n- 柔性梁弯曲变形振动学习，主线 \n\t- 广义质量 刚度矩阵及含义\n\t\n- 梳理bladed动力学框架\n\t- 子结构文献阅读\n\t- 叶片模型建模 done\n- 共旋方法学习\n- DTU 变形量计算方法学习\n\n\nP1 线性化方法编写 ing\n- 再把握理论 开启哪些自由度\n- 开始编写扰动代码\n- 形成系统矩阵\n- 分析矩阵\n\nP1 气动、多体、控制、水动联调\nP2 湍流 气动 多体 控制联调 \n- 15mw呢 yaml多个模块都需要支持\n- 更换湍流风\n- dll 32位兼容 - 江\n\nP2 停机工况等调试\n\nP1 bladed对比--稳态运行载荷，产出报告\n- 模态对比 两种描述方法不同，bladed方向更多，x y z deflection, x y z rotation，不好对比\n- 气动对比 aerodynamic info 轴向切向诱导因子，根部，尖部差距较大\n\n- 编写输出量\n\t- 方法测试 done\n\t- 批量输出编写 done\n\nP1 稳态工况前端对接\n- 是否拆分成单独的bin，等待气动完成后开始\n- 如何接收参数 配置文件 \n\nP1 专利\n\nP2 如何优雅的存储、输出结果。\nP2 yaw 自由度再bug确认 已知原理了\n","x":-597,"y":-803,"width":453,"height":457},
{"id":"c18d25521d773705","type":"text","text":"# 计划\n这周要做的3~5件重要的事情，这些事情能有效推进实现OKR。\n\nP1 必须做。P2 应该做\n\n\nP2 柔性部件 叶片、塔架变形算法 主线\n- 变形体动力学 简略看看ing\n- 柔性梁弯曲变形振动学习，主线 \n\t- 广义质量 刚度矩阵及含义\n\t\n- 梳理bladed动力学框架\n\t- 子结构文献阅读\n\t- 叶片模型建模 done\n- 共旋方法学习\n- DTU 变形量计算方法学习\n\n\nP1 线性化方法编写 ing\n- 再把握理论 开启哪些自由度 预计叶片 传动链 转速 塔架 全开\n- 开始编写扰动代码\n- 形成系统矩阵\n- 分析矩阵\n\nP1 气动、多体、控制、水动联调\nP2 湍流 气动 多体 控制联调 \n- 15mw呢 yaml多个模块都需要支持\n- 更换湍流风\n- dll 32位兼容 - 江\n\nP2 停机工况等调试\n\nP1 bladed对比--稳态运行载荷，产出报告\n- 模态对比 两种描述方法不同，bladed方向更多，x y z deflection, x y z rotation，不好对比\n- 气动对比 aerodynamic info 轴向切向诱导因子，根部，尖部差距较大\n\n- 编写输出量\n\t- 方法测试 done\n\t- 批量输出编写 done\n\nP1 稳态工况前端对接\n- 是否拆分成单独的bin，等待气动完成后开始\n- 如何接收参数 配置文件 \n\nP1 专利\n\nP2 如何优雅的存储、输出结果。\nP2 yaw 自由度再bug确认 已知原理了\n","x":-597,"y":-803,"width":453,"height":457},
{"id":"86ab96a25a3bf82e","type":"text","text":" 湍流风+ 控制的联调，bladed也算一个算例\n- 加水动的联调\n- 8月份底完成这两个\n- 9月份完成停机等工况测试\n- 10月份明阳实际机型测试","x":580,"y":-803,"width":480,"height":220},
{"id":"e355f33c92cf18ea","type":"text","text":"9月份定常计算对接前端\n非定常测试完也对接前端","x":580,"y":-500,"width":480,"height":100},
{"id":"859e6853b7f1b92b","type":"text","text":"年底考核：\n专利\n线性化模块","x":1200,"y":-803,"width":320,"height":110}

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工作总结/周报/周报98-郭翼泽.docx Normal file
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{"id":"82e0fa4b70baffed","type":"text","text":"每个工况点求稳态解","x":-300,"y":-140,"width":250,"height":60},
{"id":"d3aa69200118cea0","type":"text","text":"小扰动求A, B, C, D","x":-300,"y":0,"width":250,"height":60},
{"id":"f8e0af85235be889","type":"text","text":"A上做特征值、模态","x":-300,"y":140,"width":250,"height":60},
{"id":"03f26deb8603c7c3","type":"text","text":"输出哪些量","x":-300,"y":280,"width":250,"height":60}
{"id":"03f26deb8603c7c3","type":"text","text":"输出哪些量","x":-300,"y":280,"width":250,"height":60},
{"id":"3ad569bafe12c1a6","x":-425,"y":1020,"width":650,"height":60,"type":"text","text":"Maximum mode frequency to perturb and measure derivatives in the analysis, When using a multi-part blade, the whole\nblade modes are perturbed, The user may decide it is not necessary to analyse the higher freguency whole blade modes"},
{"id":"8ca8904fa77d3fc0","x":-425,"y":1130,"width":650,"height":60,"type":"text","text":"Number of values that each state gets perturbed to either side of the equilibrium point, Larger numbers provide more\nrobustness, Smaller numbers provide faster analysis and lower memory usage."},
{"id":"530691ed6242d413","x":-425,"y":1220,"width":650,"height":60,"type":"text","text":"Zero value states have a perturbation magnitude of this value multiplied by the absolute tolerance of the state"},
{"id":"ef6765604030b0d2","x":-425,"y":1320,"width":650,"height":60,"type":"text","text":"The magnitude of the state perturbations relative to the absolute steady-state state values"},
{"id":"667596ff1268005b","type":"text","text":"Maximum frequency to analyse","x":-845,"y":1020,"width":340,"height":60},
{"id":"871eda913aa536f2","type":"text","text":"Number of perturbation points","x":-845,"y":1130,"width":340,"height":60},
{"id":"62cc86d57a340008","type":"text","text":"Absolute tolerance perturbation scale","x":-845,"y":1220,"width":340,"height":60},
{"id":"f0a4983cbe88dea0","type":"text","text":"State relative perturbation","x":-845,"y":1320,"width":340,"height":60},
{"id":"4487cb5e83fd2407","x":300,"y":1020,"width":820,"height":60,"type":"text","text":"分析中扰动和测量导数的最大模态频率。当使用多段叶片时，整个叶片的模态会受到扰动，用户可能会认为没有必要分析更高频率的整个叶片模态。"},
{"id":"66af2e27cd04234b","x":300,"y":1130,"width":820,"height":60,"type":"text","text":"每个状态在平衡点两侧扰动到的值数量，数量越大则鲁棒性越强，数量越小则分析速度越快且内存使用量越低。"},
{"id":"be4ee34e7361d0ea","x":300,"y":1220,"width":820,"height":60,"type":"text","text":"零值状态的扰动幅度是该值乘以状态的绝对容差。"},
{"id":"83ad7939febb40fb","x":300,"y":1320,"width":820,"height":60,"type":"text","text":"状态扰动相对于绝对稳态状态值的大小"},
{"id":"57a77fa21396c8f3","x":1397,"y":971,"width":250,"height":60,"type":"text","text":"仅支持叶片稳态"},
{"id":"45093d1a52b13379","x":1397,"y":1070,"width":250,"height":60,"type":"text","text":"增加其他自由度稳态计算方法"},
{"id":"3e1714739e73cd8f","x":1780,"y":971,"width":250,"height":60,"type":"text","text":"先完成叶片的扰动"}
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