板条箱 发表于 2025-3-21 18:59:49
书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0885212<br><br> <br><br>书目名称Sensors & Instrumentation and Aircraft/Aerospace Testing Techniques Vol. 8读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0885212<br><br> <br><br>Surgeon 发表于 2025-3-21 20:45:57
Vibration Analysis of Morphing Wings,esponding to the first modes of vibration to be computed. This is done for each wing shape in order to determine and characterize the effect of wing morphing on the wing’s vibration. In particular, the shapes at which the wing will experience instability due to flutter or divergence are examined.Affiliation 发表于 2025-3-22 03:31:02
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Comparison of Calibration Techniques for Piezoelectric Force Sensors,be tested over a small percentage of its measurement range, making the technique unsuitable..A third option is to use an Impact Calibration technique similar to that of Modal Hammer Calibration. This technique offers a simple physical setup similar to that of calibrating a modal hammer using a two-c有机体 发表于 2025-3-22 11:10:30
X-57 Cruise Motor GVT Using Fixed-Base Correction Technique, the aircraft, with most of its installation hardware (wiring, baffling, sensors, etc.) attached. An impact hammer was used to provide excitation input at various locations within the tight confines of the cruise motor installation. To better support motor redesign efforts, the FBC methodology was uCULP 发表于 2025-3-22 15:19:14
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Methods and Procedures for Predicting Cable Roll-Off in Bridge-Based Sensor Measurements,nd cable resistance (.) is also explained in terms of standard specifications. Using the properly defined values for . and ., roll-off predictions are presented for measurement circuits connected by two standard cable types (paired and non-paired) and compared with roll-off measurements obtained usipatriarch 发表于 2025-3-23 05:17:24
Strain-Data-Driven Force Reconstruction Using Pseudo-Inverse Matrix,t on load prediction. Additionally, the study extends the model’s capabilities to predict temperature changes based on thermal strain inputs, achieving close alignment with actual values. In summary, this predictive model proves robust in estimating bending loads, but its sensitivity to noise, loadGanglion 发表于 2025-3-23 09:33:00
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