Vinay Dayal
Affiliations: | Iowa State University, Ames, IA, United States |
Area:
Aerospace Engineering, Applied Mechanics, Mechanical EngineeringGoogle:
"Vinay Dayal"Children
Sign in to add trainee| Sunil Kishore Chakrapani | grad student | Iowa State (Physics Tree) | |
| Leon Pickett | grad student | 2005 | Iowa State |
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Publications
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| Chakrapani SK, Dayal V. (2018) Destructive and Nondestructive Evaluation of Dry Spots in Thick Glass Fiber Reinforced Composites Applied Composite Materials. 26: 693-708 |
| Livings R, Dayal V, Barnard D. (2017) Air-Coupled Ultrasonic Resonance Imaging of Hexagonal SiC and Alumina Tiles Journal of Nondestructive Evaluation. 36 |
| Chakrapani SK, Barnard DJ, Dayal V. (2016) Influence of laminate sequence and fabric type on the inherent acoustic nonlinearity in carbon fiber reinforced composites. The Journal of the Acoustical Society of America. 139: 2310 |
| Saxena IF, Guzman N, Dayal V. (2016) NDE of bridging delamination using guided waves: Simulated and experimental results Ieee Aerospace Conference Proceedings. 2016 |
| Chakrapani SK, Barnard DJ, Dayal V. (2016) Nonlinear forced vibration of carbon fiber/epoxy prepreg composite beams: Theory and experiment Composites Part B: Engineering. 91: 513-521 |
| Livings R, Dayal V, Barnard D. (2016) Damage Detection in a Multi-Layered, Multi-Material Composite Using Air-Coupled Ultrasonic Resonance Imaging Journal of Nondestructive Evaluation. 35 |
| Chakrapani SK, Barnard D, Dayal V. (2015) Finite element simulation of core inspection in helicopter rotor blades using guided waves. Ultrasonics |
| Chakrapani SK, Barnard DJ, Dayal V. (2015) Influence of fiber orientation on the inherent acoustic nonlinearity in carbon fiber reinforced composites. The Journal of the Acoustical Society of America. 137: 617-24 |
| Chakrapani SK, Dayal V. (2014) The interaction of Rayleigh waves with delaminations in composite laminates. The Journal of the Acoustical Society of America. 135: 2646-53 |
| Chakrapani SK, Barnard D, Dayal V. (2014) Nondestructive evaluation of helicopter rotor blades using guided Lamb modes. Ultrasonics. 54: 826-33 |