항공기 복합재료 적용 시편의 압축 강도 연구

The laminated sequence and thickness of a composite structure is an important design parameter which affect the strength and impact damage. In this study, it was investigated the residual strength of carbon fiber laminate after impact damage by the experimental investigation. The tensile strength te...

Full description

Saved in:
Bibliographic Details
Published in항공우주시스템공학회지 Vol. 3; no. 1; pp. 12 - 16
Main Authors 공창덕(Changduk Kong), 박현범(Hyunbum Park), 김상훈(Sanghoon Kim), 이하승(Haseung Lee)
Format Journal Article
LanguageKorean
Published 항공우주시스템공학회 2009
Subjects
Open hole test
Compression test
Impact damage
Online AccessGet full text

Cover

Abstract The laminated sequence and thickness of a composite structure is an important design parameter which affect the strength and impact damage. In this study, it was investigated the residual strength of carbon fiber laminate after impact damage by the experimental investigation. The tensile strength test and compressive strength test were used to find the mechanical properties, previously. Impact test was performed using low-velocity drop-weight test equipment. The impact damages were finally assessed by the compressive strength test. The investigation results revealed the residual strength of the damaged specimens due to the impact damage.
AbstractList The laminated sequence and thickness of a composite structure is an important design parameter which affect the strength and impact damage. In this study, it was investigated the residual strength of carbon fiber laminate after impact damage by the experimental investigation. The tensile strength test and compressive strength test were used to find the mechanical properties, previously. Impact test was performed using low-velocity drop-weight test equipment. The impact damages were finally assessed by the compressive strength test. The investigation results revealed the residual strength of the damaged specimens due to the impact damage.
Author 이하승(Haseung Lee)
공창덕(Changduk Kong)
박현범(Hyunbum Park)
김상훈(Sanghoon Kim)
Author_xml – sequence: 1
  fullname: 공창덕(Changduk Kong)
– sequence: 2
  fullname: 박현범(Hyunbum Park)
– sequence: 3
  fullname: 김상훈(Sanghoon Kim)
– sequence: 4
  fullname: 이하승(Haseung Lee)
BookMark eNpFjMtKw0AYRgepYKx9h2xcBv65JgNuSq3XYjbdh1ymEFqjNLpwKbhTdDVUREVwVagQKJE-UzJ5BwsKfptzFodvG7Wyi0xtIItw8BwXc2ghC0tXOIICbKFOnqcRMOZSjxBiob1Gf1XLsloVdr0sGz0374v688E2H7fmZW6b-9fmcWXenm2jtfnWdlXo-unONrOiKhc7aHMUTnLV-WMbDQ_6w96RM_APj3vdgTMWwBwqZOSJmMURVh4ITqRIYkFCnnhUiVC5GKhLcDQCzBRwgjmJOBMikXEYA1DaRru_t-M0v0qDLMknwUn31CcAkoDHOWfryf8uu56m5ypJw-ByLeH0Jjjz9_sYA5OSMPoDV9Nirg
ContentType Journal Article
DBID DBRKI
TDB
JDI
DEWEY 629.1
DatabaseName DBpia
Korean Database (DBpia)
KoreaScience
DatabaseTitleList
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
DocumentTitle_FL A Study on Compressive Strength of Aircraft Composite Specimens
EISSN 2508-7150
EndPage 16
ExternalDocumentID JAKO200920855544449
NODE11049924
GroupedDBID .UV
DBRKI
TDB
JDI
ID FETCH-LOGICAL-k604-369b86c4cb1e8065296dc62a5d83e6ae7103721bf014e052152b5466d9cac0033
ISSN 1976-6300
IngestDate Fri Dec 22 12:01:15 EST 2023
Fri Oct 18 15:24:15 EDT 2024
IsOpenAccess true
IsPeerReviewed false
IsScholarly false
Issue 1
Keywords Open hole test
Compression test
Impact damage
Language Korean
LinkModel OpenURL
MergedId FETCHMERGED-LOGICAL-k604-369b86c4cb1e8065296dc62a5d83e6ae7103721bf014e052152b5466d9cac0033
Notes KISTI1.1003/JNL.JAKO200920855544449
OpenAccessLink http://click.ndsl.kr/servlet/LinkingDetailView?cn=JAKO200920855544449&dbt=JAKO&org_code=O481&site_code=SS1481&service_code=01
PageCount 5
ParticipantIDs kisti_ndsl_JAKO200920855544449
nurimedia_primary_NODE11049924
PublicationCentury 2000
PublicationDate 2009
PublicationDateYYYYMMDD 2009-01-01
PublicationDate_xml – year: 2009
  text: 2009
PublicationDecade 2000
PublicationTitle 항공우주시스템공학회지
PublicationTitleAlternate Journal of aerospace system engineering
PublicationYear 2009
Publisher 항공우주시스템공학회
Publisher_xml – name: 항공우주시스템공학회
SSID ssib044738222
ssib026777164
ssib029071394
ssib053377584
Score 1.4299161
Snippet The laminated sequence and thickness of a composite structure is an important design parameter which affect the strength and impact damage. In this study, it...
SourceID kisti
nurimedia
SourceType Open Access Repository
Publisher
StartPage 12
Title 항공기 복합재료 적용 시편의 압축 강도 연구
URI https://www.dbpia.co.kr/journal/articleDetail?nodeId=NODE11049924
http://click.ndsl.kr/servlet/LinkingDetailView?cn=JAKO200920855544449&dbt=JAKO&org_code=O481&site_code=SS1481&service_code=01
Volume 3
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnR3LahsxUCS5tDmUPukz7KE6GZd9aLUS9LJabwgpTS4u5Gb2CSXFCa196aFQ6K2lPS0tpS2FngIpGIJLvsle_0NntLazbg19GLOMR6PRSLOWRtJoRMhdTyY5NyOw3FhkNhnI2hQYi9BmaZx7lhU7OR5OfrjDtx6x7T13b2V1tea11O_F95LnS8-V_I9WAQd6xVOy_6DZOVNAAAz6hSdoGJ5_pWMatqh0qd-ioU-VQ5WrAUGV2aChmqEqIknDgMqQ-gEm-Q4VQQNRvgnWpE7zgUijhKIywHwiRG6YBjyETgNW8AVAcQAaukBToxQVm1SwispDLKZByUHdAl4msy4b6QOUSwU1GQAAsZgWxtUYf6FaUmrAh9ro7B4V8w2YhRKAvWppITHfGYmaiY81BPE1xqaSLXCR6BGCwji6sYAWGIkzEt1Cis2EElPBlVxYVZG1IQAMtCYGIquPEc5vf4Wqv5-6gFeWg7UkpvcvY-3cA3Lbf7CrA16hn6DL4IOHUDHUEbqfvghnfaLNPa8-pbUlLiuc9aGMeQ7aeLPfYL17MAWsnCmmFYF5F05GHq-Tc90-XhoBPU_NiGpfJBemsx_Dr17lS2Rl_-AyWa_FxLxC7k-K76OT4eh0YIxPhpPiqPxyPP72xii_viw_Hhnl60-Tt6fl5w9GWRTlj8IYDYrxu1dG-X4wGh5fJe3NsB1sNadXfDT3OW7JcRkLnrAktjLc4bclTxNuR24qnIxHmYenWG0rzmEin-Exc9eOXcZ5KpMowWsIr5G17kE3u06MXJoyytIkZ57J4phLS2bCjjIMmRDnsbxBNnQjdLrpsyedJc0PBPPW6RxWoV46O7utEAxkJqXNbv6Jwy1yvtprxAW622St97Sf3QGTtRdvaJ3-BHZucag
link.rule.ids 230,315,786,790,891,4043
linkProvider ISSN International Centre
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=%ED%95%AD%EA%B3%B5%EA%B8%B0+%EB%B3%B5%ED%95%A9%EC%9E%AC%EB%A3%8C+%EC%A0%81%EC%9A%A9+%EC%8B%9C%ED%8E%B8%EC%9D%98+%EC%95%95%EC%B6%95+%EA%B0%95%EB%8F%84+%EC%97%B0%EA%B5%AC&rft.jtitle=%ED%95%AD%EA%B3%B5%EC%9A%B0%EC%A3%BC%EC%8B%9C%EC%8A%A4%ED%85%9C%EA%B3%B5%ED%95%99%ED%9A%8C%EC%A7%80&rft.au=%EA%B3%B5%EC%B0%BD%EB%8D%95&rft.au=%EB%B0%95%ED%98%84%EB%B2%94&rft.au=%EA%B9%80%EC%83%81%ED%9B%88&rft.au=%EC%9D%B4%ED%95%98%EC%8A%B9&rft.date=2009&rft.issn=1976-6300&rft.volume=3&rft.issue=1&rft.spage=12&rft.epage=16&rft.externalDBID=n%2Fa&rft.externalDocID=JAKO200920855544449
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1976-6300&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1976-6300&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1976-6300&client=summon