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Shock & vibration, aircraft/aerospace, energy harvesting, acoustics & optics. . Volume 9 : proceedings of the 35th IMAC, a Conference and Exposition on Structural Dynamics 2017 / Julie M. Harvie, Javad Baqersad, editors.

By: (35th : International Modal Analysis Conference ((35th : 2017 : Garden Grove, Calif.))
Contributor(s): Baqersad, Javad,, editor literario | Harvie, Julie M.,, editor literario
Material type: materialTypeLabelE-bookSeries: (Conference proceedings of the Society for Experimental Mechanics series).Publisher: Cham, Switzerland : Springer, 2017Description: 1 recurso en línea.ISBN: 3319547356; 9783319547350.Subject: Almacenamiento de energíaOnline resources: Acceso a este recurso digital (usuarios Universidad Europea de Madrid)Digital Resources
Contents:
Preface; Contents; 1 Scaling up of the Impedance-Matched Multi-Axis Test (IMMAT) Technique; 1.1 Introduction; 1.2 The Modal Analysis Test Vehicle; 1.3 Gathering the "Truth Data"; 1.4 Deriving a Test Specification (Target Spectra) for an IMMAT Test; 1.5 Planning the IMMAT Test; 1.6 The IMMAT Test; 1.7 Results and Discussion; 1.7.1 Test 1; 1.7.2 Test 2; 1.8 Conclusions; References; 2 6-DOF Shaker Test Input Derivation from Field Test; 2.1 Introduction; 2.1.1 Overall Concept; 2.2 Deriving the Transmissibility Function; 2.3 Deriving the 6-DOF Shaker Table Input Given Flight Data.
2.3.1 Method 1: PINV2.3.2 Method 2: ZINV; 2.3.3 Method 3: Scaling; 2.3.4 Method 4: Smallwood-Cap; 2.4 Comparison Metric for Methods; 2.4.1 Comparison of Inputs; 2.4.2 Comparison of Predicted Responses to Actual Field Responses; 2.5 Conclusions; References; 3 Frequency Based Spatial Damping Identification-Theoretical and Experimental Comparison; 3.1 Introduction; 3.2 Theoretical Background; 3.3 Experiments; 3.3.1 Measurement Setup; 3.4 Analysis and Discussion; 3.4.1 Modal Incompleteness; 3.4.2 Spatial Incompleteness; 3.4.3 Damping Treatment Effect on Spatial Location; 3.5 Conclusion.
5.1 Introduction5.1.1 Motivation; 5.1.2 Dynamic Model and System Input-Output Theory; 5.2 Background; 5.2.1 Video Processing: Automated Video Extraction; 5.2.2 Regularization Methods; 5.3 Experimental Setup; 5.3.1 Laboratory Setup; 5.3.2 Establishing Dynamic Model; 5.3.3 Inverse Load ID; 5.4 Results; 5.4.1 FEA Model; 5.4.2 Inverse Load ID; 5.5 Conclusion; References; 6 Research of Under-Sampling Technique for Digital Image Correlation in Vibration Measurement; 6.1 Introduction; 6.2 Estimate Depth of Workpiece with a Stereo Camera; 6.3 Undersampling Technique; 6.4 Timestamp Optimization.
6.5 Experimental Verification6.6 Conclusion; References; 7 Nonlinear Dynamic Analysis of a Thermally Buckled Aircraft Panel Using NNMs; 7.1 Introduction; 7.2 Theoretical Development; 7.2.1 Review of Reduced Order Modeling; 7.2.2 Review of Nonlinear Normal Modes; 7.3 Application to FE of an Aircraft Ramp Panel; 7.4 Conclusions; 7.5 Future Work; References; 8 Empirically-Derived, Constitutive Damping Model for Cellular Silicone; Nomenclature; 8.1 Background; 8.2 Experiment; 8.2.1 Test Fixture Design; 8.2.2 Test Set-Up; 8.2.3 Linear Modal Analysis Results.
Abstract: Shock & Vibration, Aircraft/Aerospace and Energy Harvesting, Volume 9: Proceedings of the 35th IMAC, A Conference and Exposition on Structural Dynamics, 2017, the ninth volume of ten from the Conference brings together contributions to this important area of research and engineering. The collection presents early findings and case studies on fundamental and applied aspects of Shock & Vibration, Aircraft/Aerospace and Energy Harvesting including papers on: Shock & Vibration Testing Aircraft/Aerospace Applications Optical Techniques: Digital Image Correlation Vibration Suppression & Control Damage Detection Energy Harvesting.
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Holdings
Item type Current library Collection Call number Status Date due Barcode Item holds
LIBRO-E NO PRÉSTAMO LIBRO-E NO PRÉSTAMO Madrid Digital Acceso Electrónico (UEM) Ciencias e Ingeniería TA654 .S563 2017 EB (Browse shelf(Opens below)) Acceso electrónico eBook.20023438
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SpringerLink Springer Engineering eBooks 2017 English+International

Preface; Contents; 1 Scaling up of the Impedance-Matched Multi-Axis Test (IMMAT) Technique; 1.1 Introduction; 1.2 The Modal Analysis Test Vehicle; 1.3 Gathering the "Truth Data"; 1.4 Deriving a Test Specification (Target Spectra) for an IMMAT Test; 1.5 Planning the IMMAT Test; 1.6 The IMMAT Test; 1.7 Results and Discussion; 1.7.1 Test 1; 1.7.2 Test 2; 1.8 Conclusions; References; 2 6-DOF Shaker Test Input Derivation from Field Test; 2.1 Introduction; 2.1.1 Overall Concept; 2.2 Deriving the Transmissibility Function; 2.3 Deriving the 6-DOF Shaker Table Input Given Flight Data.

2.3.1 Method 1: PINV2.3.2 Method 2: ZINV; 2.3.3 Method 3: Scaling; 2.3.4 Method 4: Smallwood-Cap; 2.4 Comparison Metric for Methods; 2.4.1 Comparison of Inputs; 2.4.2 Comparison of Predicted Responses to Actual Field Responses; 2.5 Conclusions; References; 3 Frequency Based Spatial Damping Identification-Theoretical and Experimental Comparison; 3.1 Introduction; 3.2 Theoretical Background; 3.3 Experiments; 3.3.1 Measurement Setup; 3.4 Analysis and Discussion; 3.4.1 Modal Incompleteness; 3.4.2 Spatial Incompleteness; 3.4.3 Damping Treatment Effect on Spatial Location; 3.5 Conclusion.

5.1 Introduction5.1.1 Motivation; 5.1.2 Dynamic Model and System Input-Output Theory; 5.2 Background; 5.2.1 Video Processing: Automated Video Extraction; 5.2.2 Regularization Methods; 5.3 Experimental Setup; 5.3.1 Laboratory Setup; 5.3.2 Establishing Dynamic Model; 5.3.3 Inverse Load ID; 5.4 Results; 5.4.1 FEA Model; 5.4.2 Inverse Load ID; 5.5 Conclusion; References; 6 Research of Under-Sampling Technique for Digital Image Correlation in Vibration Measurement; 6.1 Introduction; 6.2 Estimate Depth of Workpiece with a Stereo Camera; 6.3 Undersampling Technique; 6.4 Timestamp Optimization.

6.5 Experimental Verification6.6 Conclusion; References; 7 Nonlinear Dynamic Analysis of a Thermally Buckled Aircraft Panel Using NNMs; 7.1 Introduction; 7.2 Theoretical Development; 7.2.1 Review of Reduced Order Modeling; 7.2.2 Review of Nonlinear Normal Modes; 7.3 Application to FE of an Aircraft Ramp Panel; 7.4 Conclusions; 7.5 Future Work; References; 8 Empirically-Derived, Constitutive Damping Model for Cellular Silicone; Nomenclature; 8.1 Background; 8.2 Experiment; 8.2.1 Test Fixture Design; 8.2.2 Test Set-Up; 8.2.3 Linear Modal Analysis Results.

Shock & Vibration, Aircraft/Aerospace and Energy Harvesting, Volume 9: Proceedings of the 35th IMAC, A Conference and Exposition on Structural Dynamics, 2017, the ninth volume of ten from the Conference brings together contributions to this important area of research and engineering. The collection presents early findings and case studies on fundamental and applied aspects of Shock & Vibration, Aircraft/Aerospace and Energy Harvesting including papers on: Shock & Vibration Testing Aircraft/Aerospace Applications Optical Techniques: Digital Image Correlation Vibration Suppression & Control Damage Detection Energy Harvesting.

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