Sensors and instrumentation, aircraft/aerospace, energy harvesting & dynamic environment testing. Volume 7 : proceedings of the 37th IMAC, a conference and exposition on structural dynamics 2019 / editors, Chad Walber, Patrick Walter and Steve Seidlitz.

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Bibliographic Details
Online Access: Full Text (via Springer)
Corporate Author: International Modal Analysis Conference Orlando, Florida
Other Authors: Walber, Chad (Editor), Walter, Patrick (Director), Seidlitz, Steve (Editor)
Format: Conference Proceeding eBook
Language:English
Published: Cham, Switzerland : Springer, 2019.
Series:Conference proceedings of the Society for Experimental Mechanics series.
Subjects:

MARC

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245 1 0 |a Sensors and instrumentation, aircraft/aerospace, energy harvesting & dynamic environment testing.  |n Volume 7 :  |b proceedings of the 37th IMAC, a conference and exposition on structural dynamics 2019 /  |c editors, Chad Walber, Patrick Walter and Steve Seidlitz. 
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505 0 |a Intro; Preface; Contents; 1 Historical Review of "Building Block Approach" in Validation for Human Space Flight; 1.1 Introduction; 1.2 Building Blocks and the Integrated System; 1.3 Saturn V Experience (1960s); 1.4 STS Experience (1970s); 1.5 Experience to Date and Plans for the Integrated Space Launch System (SLS); 1.6 Conclusion; References; 2 Analytically Investigating Impedance-Matching Test Fixtures; 2.1 Introduction; 2.1.1 Box Assembly and Removable Component; 2.1.2 N+1 Fixtures; 2.1.3 Excitation Methods; 2.1.4 Control Method Used in this Paper; 2.2 "Truth" Data. 
505 8 |a 2.3 Single Axis Shaker Excitation2.3.1 Method; 2.3.2 Results; 2.4 Six DoF Shaker Excitation; 2.4.1 Method; 2.4.2 Results; 2.5 Multi-Shaker Excitation; 2.5.1 Method; 2.5.2 Results; 2.6 Conclusions; References; 3 Harmonic Forcing of Damped Non-homogeneous Elastic Rods; Nomenclature; 3.1 Introduction; 3.2 Basic Structure; 3.3 Analytic Solutions; 3.3.1 Constant Spatial Force; 3.3.1.1 Free-Fixed Boundary Conditions; 3.3.1.2 Fixed-Fixed Boundary Conditions; 3.4 Continuous Variation Model; 3.5 Numerical Examples; 3.5.1 Free-Fixed Boundary Conditions; 3.5.2 Fixed-Fixed Boundary Conditions. 
505 8 |a 3.6 ConclusionsReferences; 4 Effects of Multi-Axial versus Single-Axial Excitation of Jointed Systems; 4.1 Introduction; 4.2 Experiment and Results; 4.2.1 Multisine Test; 4.2.2 Steady State Sine Test; 4.3 Conclusion; References; 5 Quantifying the Effect of Component Inertial Properties on System Level Dynamics; 5.1 Introduction; 5.2 Model Setup & Development; 5.3 Modal Results; 5.4 Frequency Response Function & Component Test Results; 5.4.1 Plates: Assembly Level Responses; 5.4.2 Small Box Component: Assembly and Component Level Responses. 
505 8 |a 5.4.3 Beam Component: Assembly and Component Level Responses5.5 Conclusion; References; 6 A Method for Determining Impact Force for Single and Tri Axis Resonant Plate Shock Simulations; 6.1 Introduction; 6.2 Background; 6.3 Analysis; 6.4 Conclusion; References; 7 Non-stationarity and non-Gaussianity in Vibration Fatigue; 7.1 Introduction; 7.2 Background; 7.2.1 Non-Gaussianity vs. Non-stationarity; 7.3 Non-stationarity Index; 7.4 Conclusions; References; 8 Use of Topology Optimization to Design Shock and Vibration Test Fixtures; Nomenclature; 8.1 Introduction; 8.2 Theory. 
505 8 |a 8.3 Topology Optimization8.4 Case Study; 8.4.1 Creating an Optimized Test Fixture; 8.4.2 Comparing the Optimized and Rigid Test Fixtures; 8.5 Conclusion; References; 9 Electromechanical Impedance Method for Applications in Boundary Condition Replication; 9.1 Introduction; 9.2 Background; 9.3 Analysis; 9.4 Conclusion; References; 10 Latest Design Trends in Modal Accelerometers for Aircraft Ground Vibration Testing; 10.1 Introduction; 10.2 Requirements of Accelerometers for Large Structure Modal Testing; 10.3 Accelerometer Technologies for Modal Applications. 
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