Author: Beth Doll
Publisher:
ISBN:
Category : Carbon composites
Languages : en
Pages : 74
Book Description
Ultrasonic Attenuation as a Method of Nondestructive Evaluation of Graphite Epoxy Composites Undergoing Compression-compression Fatigue
Author: Beth Doll
Publisher:
ISBN:
Category : Carbon composites
Languages : en
Pages : 74
Book Description
Publisher:
ISBN:
Category : Carbon composites
Languages : en
Pages : 74
Book Description
Ultrasonic Attenuation as an Indicator of Fatigue Life of Graphite/epoxy Fiber Composite
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Ultrasonic Attenuation as an Indicator of Fatigue Life of Granite/epoxy Fiber Composite
Author: James H. Williams
Publisher:
ISBN:
Category : Quality control
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Quality control
Languages : en
Pages : 28
Book Description
NASA Contractor Report
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 512
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 512
Book Description
Materials Evaluation
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 886
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 886
Book Description
Ultrasonic Attenuation and Velocity in AS/3501-6 Graphite
Author: James H. Williams
Publisher:
ISBN:
Category : Sound
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Sound
Languages : en
Pages : 44
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1282
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1282
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Ultrasonic Attenuation and Velocity in As/3501-6 Graphite/Epoxy Fiber Composite
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725052666
Category :
Languages : en
Pages : 36
Book Description
The ultrasonic group velocity and attenuation were measured as a function of frequency for longitudinal and shear waves in the epoxy matrix (3501-6) and in the principal directions of the unidirectional graphite/epoxy composite (AS/3501-6). Tests were conducted in the frequency ranges 0.25 Mz to 14 MHz and 0.5 Mz to 3 MHz for longitudinal and shear wave modes, respectively. The attenuation increased with frequency for all wave modes, but the group velocity was independent of frequency for all wave modes. The effects of pressure and couplant at the transducer-specimen interface were studied and it was found that for each transducer type there exists a frequency dependent 'saturation pressure' corresponding to the maximum output signal amplitude. Williams, J. H., Jr. and Nayebhashemi, H. and Lee, S. S. Unspecified Center NASA-CR-3180 NSG-3210...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725052666
Category :
Languages : en
Pages : 36
Book Description
The ultrasonic group velocity and attenuation were measured as a function of frequency for longitudinal and shear waves in the epoxy matrix (3501-6) and in the principal directions of the unidirectional graphite/epoxy composite (AS/3501-6). Tests were conducted in the frequency ranges 0.25 Mz to 14 MHz and 0.5 Mz to 3 MHz for longitudinal and shear wave modes, respectively. The attenuation increased with frequency for all wave modes, but the group velocity was independent of frequency for all wave modes. The effects of pressure and couplant at the transducer-specimen interface were studied and it was found that for each transducer type there exists a frequency dependent 'saturation pressure' corresponding to the maximum output signal amplitude. Williams, J. H., Jr. and Nayebhashemi, H. and Lee, S. S. Unspecified Center NASA-CR-3180 NSG-3210...
Implications of Ultrasonic Attenuation to Nondestructive Testing
Author: J. K. White
Publisher:
ISBN:
Category : Nuclear reactions
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Nuclear reactions
Languages : en
Pages : 24
Book Description
Ultrasonic Nondestructive Evaluation, Microstructure, and Mechanical Property Interrelations
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description