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Ultrasonic Guided Waves Test Method for Blunt Impact Damage Assessment on Composite Aircraft Structures
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Copyright Title

Ultrasonic Guided Waves Test Method for Blunt Impact Damage Assessment on Composite Aircraft Structures

Status

Published

on 23 Apr 2020
Year of Creation
2020
Copyright Claimant
Hyung Suk Kim
Registration Number
TX0008868291
on 23 Apr 2020

Copyright Summary


The U.S. Copyright record (Registration Number: TX0008868291) dated 23 Apr 2020, pertains to an electronic file (eService) titled "Ultrasonic Guided Waves Test Method for Blunt Impact Damage Assessment on Composite Aircraft Structures" created in 2020. The copyright holder is Hyung Suk Kim, known for their creative contributions in text registration. For any inquiries concerning this copyrighted material, kindly reach out to Hyung Suk Kim.

Copyright Details


Copyright Claimant
Hyung Suk Kim

Application Details


Registration Number
TX0008868291
Registration Date
4/23/2020
Year of Creation
2020
Agency Marc Code
DLC-CO
Record Status
New
Physical Description
Electronic file (eService)
First Publication Nation
United States

Personal Authors


Notes


Rights Note: Mark Dill, ProQuest, LLC, 789 E. Eisenhower Parkway, Ann Arbor, MI, 48108-3218, United States, (800) 521-0600, disspub@proquest.com

Statements


Application Title Statement: Ultrasonic Guided Waves Test Method for Blunt Impact Damage Assessment on Composite Aircraft Structures
Author Statement: Hyung Suk Kim Citizenship: not known Authorship: text
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