vault backup: 2025-09-25 09:08:18
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.obsidian/plugins/copilot/data.json
vendored
34
.obsidian/plugins/copilot/data.json
vendored
@ -139,23 +139,6 @@
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"stream": true,
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"enableCors": true
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},
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{
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"name": "gemini-2.5-flash",
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"provider": "google",
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"enabled": true,
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"isBuiltIn": false,
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"baseUrl": "http://60.205.246.14:8000",
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"apiKey": "gyz",
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"isEmbeddingModel": false,
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"capabilities": [
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"reasoning",
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"vision",
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"websearch"
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],
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"stream": true,
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"displayName": "gemini-2.5-flash",
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"enableCors": true
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},
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{
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"name": "gemini-2.5-pro",
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"provider": "google",
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@ -172,6 +155,23 @@
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"stream": true,
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"displayName": "gemini-2.5-pro",
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"enableCors": true
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},
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{
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"name": "gemini-2.5-flash",
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"provider": "google",
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"enabled": true,
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"isBuiltIn": false,
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"baseUrl": "",
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"apiKey": "AIzaSyAnULu8WrFeKeOpW2SoJdqXGu4FrDcyB2I",
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"isEmbeddingModel": false,
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"capabilities": [
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"reasoning",
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"vision",
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"websearch"
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],
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"stream": true,
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"displayName": "gemini-2.5-flash",
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"enableCors": true
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}
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],
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"activeEmbeddingModels": [
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@ -1269,10 +1269,10 @@ $$
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v_{6}=\left({\frac{v_{1}}{v_{0}}}\right)^{6}\,v_{0}=\left({\frac{4}{5}}\right)^{6}\,(0.20)=0.0524\,i n\quad[0.1331\;c m]
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$$
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## Overcritically-Damped Systems
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## Overcritically-Damped Systems过阻尼系统
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Although it is very unusual under normal conditions to have overcriticallydamped structural systems, they do sometimes occur as mechanical systems; therefore, it is useful to carry out the response analysis of an overcritically-damped system to make this presentation complete. In this case having $\xi\equiv c/c_{c}>1$ , it is convenient to write Eq. (2-39) in the form
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尽管在正常条件下出现过临界阻尼结构系统非常罕见,但它们有时确实作为机械系统出现;因此,进行过临界阻尼系统的响应分析对于使本次论述完整是有益的。在这种阻尼比 $\xi\equiv c/c_{c}>1$ 的情况下,将方程 (2-39) 写成以下形式是方便的。
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$$
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s_{1,2}=-\xi\omega\pm\omega\sqrt{\xi^{2}-1}=-\xi\omega\pm\hat{\omega}
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$$
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@ -1284,13 +1284,13 @@ $$
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$$
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Substituting the two values of $s$ given by Eq. (2-60) into Eq. (2-21) and simplifying leads eventually to
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将由式 (2-60) 给出的 $s$ 的两个值代入式 (2-21) 并进行简化,最终可得
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$$
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v(t)=[A\,\sinh\hat{\omega}t+B\,\cosh\hat{\omega}t]\,\,\exp(-\xi\omega t)
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$$
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in which the real constants $A$ and $B$ can be evaluated using the initial conditions $v(0)$ and $\dot{v}(0)$ . It is easily shown from the form of Eq. (2-62) that the response of an overcritically-damped system is similar to the motion of a critically-damped system as shown in Fig. 2-9; however, the asymptotic return to the zero-displacement position is slower depending upon the amount of damping.
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其中实常数 $A$ 和 $B$ 可以利用初始条件 $v(0)$ 和 $\dot{v}(0)$ 来确定。从方程 (2-62) 的形式可以很容易地看出,过阻尼系统的响应与临界阻尼系统的运动相似,如图 2-9 所示;然而,渐近返回到零位移位置的速度会变慢,这取决于阻尼量。
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# PROBLEMS
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2-1. The weight $W$ of the building of Fig. E2-1 is $200\,k i p s$ and the building is set into free vibration by releasing it (at time $t=0$ ) from a displacement of $1.20\;i n$ . If the maximum displacement on the return swing is $0.86\;i n$ at time $t=0.64~s e c$ , determine:
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78
多体+耦合求解器/输出量及输出与bladed对比.md
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78
多体+耦合求解器/输出量及输出与bladed对比.md
Normal file
@ -0,0 +1,78 @@
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fast
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tip motions ---Blade deflections
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| Bladed | FAST |
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| ------------------------------------------ | ---- |
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| x deflection(perpendicular to rotor plane) | |
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| y deflection(in rotor plane) | |
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| z deflection(in rotor plane) | |
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| rotation about x(plane) | × |
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| rotation about y(plane) | × |
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| rotation about z(plane) | × |
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| x deflection(blade root axes) | |
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| y deflection(blade root axes) | |
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| z deflection(blade root axes) | |
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| rotation about x(blade root axes) | × |
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| rotation about y(blade root axes) | × |
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| rotation about z(blade root axes) | × |
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local span motions ---Blade deflections
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pitch motions ---pitch system
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teeter motions ---pass
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shaft motions ---generator variables
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| LSSTipPxa | LSSTipPxs, LSSTipP, Azimuth | Rotor azimuth angle (position) | About the xa- and xs-axes | (deg) |
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| --------- | ---------------------------- | ------------------------------------------------------------------------------------------------- | -------------------------------------------- | --------- |
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| LSSTipVxa | LSSTipVxs, LSSTipV, RotSpeed | Rotor azimuth angular speed | About the xa- and xs-axes | (rpm) |
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| LSSTipAxa | LSSTipAxs, LSSTipA, RotAccel | Rotor azimuth angular acceleration | About the xa- and xs-axes | (deg/s^2) |
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| LSSGagPxa | LSSGagPxs, LSSGagP | Low-speed shaft strain gage azimuth angle (position) (on the gearbox side of the low-speed shaft) | About the xa- and xs-axes | (deg) |
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| LSSGagVxa | LSSGagVxs, LSSGagV | Low-speed shaft strain gage angular speed (on the gearbox side of the low-speed shaft) | About the xa- and xs-axes | (rpm) |
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| LSSGagAxa | LSSGagAxs, LSSGagA | Low-speed shaft strain gage angular acceleration (on the gearbox side of the low-speed shaft) | About the xa- and xs-axes | (deg/s^2) |
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| HSShftV | GenSpeed | Angular speed of the high-speed shaft and generator | Same sign as LSSGagVxa / LSSGagVxs / LSSGagV | (rpm) |
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| HSShftA | GenAccel | Angular acceleration of the high-speed shaft and generator | Same sign as LSSGagAxa / LSSGagAxs / LSSGagA | (deg/s^2) |
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nacelle imu motions --- nacelle motion
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rotor-furl motions --- pass
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tail-furl motions --- pass
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nacelle yaw motions --- nacelle motion
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Tower-Top / Yaw Bearing Motions --- nacelle motion
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Local Tower Motions
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Platform Motions
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Blade 1 Root Loads --- hub loads rotating gl coordinates
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Blade 2 Root Loads
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Blade 3 Root Loads
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Blade 1 Local Span Loads --- blade loads
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Blade 2 Local Span Loads
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Blade 3 Local Span Loads
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Hub and Rotor Loads
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Shaft Strain Gage Loads
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High-Speed Shaft Loads
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Rotor-Furl Bearing Loads
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Tail-Furl Bearing Loads
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Tower-Top / Yaw Bearing Loads
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Tower Base Loads --- foundation loads
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Local Tower Loads
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Internal Degrees of Freedom
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