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

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

Label
Shock & vibration, aircraft/aerospace, energy harvesting, acoustics & optics : proceedings of the 35th IMAC, a Conference and Exposition on Structural Dynamics 2017, Volume 9
Title
Shock & vibration, aircraft/aerospace, energy harvesting, acoustics & optics
Title remainder
proceedings of the 35th IMAC, a Conference and Exposition on Structural Dynamics 2017
Title number
Volume 9
Statement of responsibility
Julie M. Harvie, Javad Baqersad, editors
Creator
Contributor
Editor
Subject
Genre
Language
eng
Member of
Cataloging source
N$T
Dewey number
620.1/074
Index
no index present
LC call number
TA654
LC item number
.I58 2017eb
Literary form
non fiction
http://bibfra.me/vocab/lite/meetingDate
2017
http://bibfra.me/vocab/lite/meetingName
International Modal Analysis Conference
Nature of contents
dictionaries
http://library.link/vocab/relatedWorkOrContributorName
  • Harvie, Julie M.
  • Baqersad, Javad
Series statement
Conference proceedings of the Society for Experimental Mechanics series
http://library.link/vocab/subjectName
  • Structural dynamics
  • Aerospace engineering
  • Energy harvesting
Label
Shock & vibration, aircraft/aerospace, energy harvesting, acoustics & optics : proceedings of the 35th IMAC, a Conference and Exposition on Structural Dynamics 2017, Volume 9, Julie M. Harvie, Javad Baqersad, editors
Instantiates
Publication
Antecedent source
unknown
Carrier category
online resource
Carrier category code
cr
Carrier MARC source
rdacarrier
Color
multicolored
Content category
text
Content type code
txt
Content type MARC source
rdacontent
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
Dimensions
unknown
Extent
1 online resource.
File format
unknown
Form of item
online
Isbn
9783319547350
Level of compression
unknown
Media category
computer
Media MARC source
rdamedia
Media type code
c
Quality assurance targets
not applicable
Reformatting quality
unknown
Sound
unknown sound
Specific material designation
remote
System control number
ocn982958163
Label
Shock & vibration, aircraft/aerospace, energy harvesting, acoustics & optics : proceedings of the 35th IMAC, a Conference and Exposition on Structural Dynamics 2017, Volume 9, Julie M. Harvie, Javad Baqersad, editors
Publication
Antecedent source
unknown
Carrier category
online resource
Carrier category code
cr
Carrier MARC source
rdacarrier
Color
multicolored
Content category
text
Content type code
txt
Content type MARC source
rdacontent
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
Dimensions
unknown
Extent
1 online resource.
File format
unknown
Form of item
online
Isbn
9783319547350
Level of compression
unknown
Media category
computer
Media MARC source
rdamedia
Media type code
c
Quality assurance targets
not applicable
Reformatting quality
unknown
Sound
unknown sound
Specific material designation
remote
System control number
ocn982958163

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