Matches in SemOpenAlex for { <https://semopenalex.org/work/W4361212976> ?p ?o ?g. }
Showing items 1 to 59 of
59
with 100 items per page.
- W4361212976 endingPage "012006" @default.
- W4361212976 startingPage "012006" @default.
- W4361212976 abstract "Abstract The extensive use of composites in aircraft leads to the problem of damage tolerance after low-speed impact. It is necessary to consider not only the change of mechanical properties but also the change of work properties such as air tightness. In this paper, the damage morphology and air tightness of a typical composite stiffened panel subjected to low-speed impact were experimentally studied. The damage initiation and propagation and the change of air tightness after impact, static compression and compression fatigue were analyzed respectively. It is found from the test that after 120% ultimate load condition and 100,000 times constant amplitude fatigue load condition, the impact damage does not expand, and the air tightness is good and no obvious leakage is observed, indicating that the structural design meets the requirements of damage tolerance and air tightness." @default.
- W4361212976 created "2023-03-31" @default.
- W4361212976 creator A5008960297 @default.
- W4361212976 creator A5010898755 @default.
- W4361212976 creator A5022499603 @default.
- W4361212976 creator A5057718629 @default.
- W4361212976 creator A5068884694 @default.
- W4361212976 date "2023-03-01" @default.
- W4361212976 modified "2023-09-26" @default.
- W4361212976 title "Experimental research on damage tolerance and air tightness of typical composite panels" @default.
- W4361212976 doi "https://doi.org/10.1088/1742-6596/2459/1/012006" @default.
- W4361212976 hasPublicationYear "2023" @default.
- W4361212976 type Work @default.
- W4361212976 citedByCount "0" @default.
- W4361212976 crossrefType "journal-article" @default.
- W4361212976 hasAuthorship W4361212976A5008960297 @default.
- W4361212976 hasAuthorship W4361212976A5010898755 @default.
- W4361212976 hasAuthorship W4361212976A5022499603 @default.
- W4361212976 hasAuthorship W4361212976A5057718629 @default.
- W4361212976 hasAuthorship W4361212976A5068884694 @default.
- W4361212976 hasBestOaLocation W43612129761 @default.
- W4361212976 hasConcept C104779481 @default.
- W4361212976 hasConcept C127413603 @default.
- W4361212976 hasConcept C159985019 @default.
- W4361212976 hasConcept C180016635 @default.
- W4361212976 hasConcept C18762648 @default.
- W4361212976 hasConcept C192562407 @default.
- W4361212976 hasConcept C2776656632 @default.
- W4361212976 hasConcept C66938386 @default.
- W4361212976 hasConcept C78519656 @default.
- W4361212976 hasConceptScore W4361212976C104779481 @default.
- W4361212976 hasConceptScore W4361212976C127413603 @default.
- W4361212976 hasConceptScore W4361212976C159985019 @default.
- W4361212976 hasConceptScore W4361212976C180016635 @default.
- W4361212976 hasConceptScore W4361212976C18762648 @default.
- W4361212976 hasConceptScore W4361212976C192562407 @default.
- W4361212976 hasConceptScore W4361212976C2776656632 @default.
- W4361212976 hasConceptScore W4361212976C66938386 @default.
- W4361212976 hasConceptScore W4361212976C78519656 @default.
- W4361212976 hasIssue "1" @default.
- W4361212976 hasLocation W43612129761 @default.
- W4361212976 hasOpenAccess W4361212976 @default.
- W4361212976 hasPrimaryLocation W43612129761 @default.
- W4361212976 hasRelatedWork W1484362229 @default.
- W4361212976 hasRelatedWork W1999605826 @default.
- W4361212976 hasRelatedWork W2315337917 @default.
- W4361212976 hasRelatedWork W2347469006 @default.
- W4361212976 hasRelatedWork W2367936634 @default.
- W4361212976 hasRelatedWork W2900524175 @default.
- W4361212976 hasRelatedWork W3043268847 @default.
- W4361212976 hasRelatedWork W3048672776 @default.
- W4361212976 hasRelatedWork W3142048519 @default.
- W4361212976 hasRelatedWork W2463824739 @default.
- W4361212976 hasVolume "2459" @default.
- W4361212976 isParatext "false" @default.
- W4361212976 isRetracted "false" @default.
- W4361212976 workType "article" @default.