Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Hsi-Yung T. Wu"'
Publikováno v:
Journal of Aircraft. 58:580-590
Hybrid wing body is a fuel-efficient aircraft configuration where the pressurized center section is confined by almost-flat panels jointed at right angles. The combination of internal pressure and ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::709827ba66a611cd98d838e00e3cd4db
https://doi.org/10.2514/1.c035911
https://doi.org/10.2514/1.c035911
Publikováno v:
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The Environmentally Responsible Aviation Project aimed to develop aircraft technologies enabling significant fuel burn and community noise reductions. Small incremental changes to the conventional metallic alloy-based ‘tube and wing’ configuratio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06a8b2092c5ebea8800e11e4deb43869
https://doi.org/10.2514/6.2016-2176
https://doi.org/10.2514/6.2016-2176
Publikováno v:
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9033b8af96732a7ef70d4699fdc0a80
https://doi.org/10.2514/6.2016-2177
https://doi.org/10.2514/6.2016-2177
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The Environmentally Responsible Aviation Project aims to develop aircraft technologies enabling significant fuel burn and community noise reductions. Small incremental changes to the conventional metallic alloy-based 'tube and wing' configuration are
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ae4ee5136e217ab22f6483aa51a6d0b
https://doi.org/10.2514/6.2014-1064
https://doi.org/10.2514/6.2014-1064
Publikováno v:
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The hybrid wing body center section test article is an all-composite structure made of crown, floor, keel, bulkhead, and rib panels utilizing the Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS) design concept. The primary goal of this te
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f7ef0f847d48263678e5cc64470dd7e
https://doi.org/10.2514/6.2013-1734
https://doi.org/10.2514/6.2013-1734
Publikováno v:
Composite Structures. 25:267-275
A parametric study of residual strength and stiffness for low-velocity impact damaged composites was performed. Possible compression after impact failure mechanisms, which may be caused by stiffness and strength degradation inside the damage region,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b31fa251d345b002558914f97904f818
https://doi.org/10.1016/0263-8223(93)90173-n
https://doi.org/10.1016/0263-8223(93)90173-n
Publikováno v:
Journal of Composite Materials. 25:1012-1038
An investigation consisting of both analysis and experiments was performed to study impact damage mechanisms and mechanics of laminated composites subjected to low-velocity impact. In order to fundamentally understand the impact damage of laminated c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::674cd0d8084251b3f6f9e0d858af653c
https://doi.org/10.1177/002199839102500804
https://doi.org/10.1177/002199839102500804
Autor:
Fu-Kuo Chang, Hsi-Yung T. Wu
Publikováno v:
Computers & Structures. 31:453-466
The dynamic response of a composite laminate plate to transverse impact loading is simulated numerically. An FEM scheme based on an eight-point brick element and three-dimensional linear elasticity theory is employed, assuming that the laminate layer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::101b708caa78fe9b79dcae3013afd78f
https://doi.org/10.1016/0045-7949(89)90393-3
https://doi.org/10.1016/0045-7949(89)90393-3
Autor:
Hsi-Yung T. Wu, George S. Springer
Publikováno v:
Journal of Composite Materials. 22:518-532
Tests were performed measuring the locations and extents of delaminations and matrix crackings in 3 inches by 3 inches Fiberite T300/934 graphite/epoxy plates impacted by 1/2 inch diameter aluminum spheres. Plates with six ply orientations were teste
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41b6cc71762f7e97fe3abacff7f76418
https://doi.org/10.1177/002199838802200602
https://doi.org/10.1177/002199838802200602
Autor:
George S. Springer, Hsi-Yung T. Wu
Publikováno v:
Journal of Composite Materials. 22:533-560
A method is presented for calculating the locations and sizes of delaminations which oc cur in a rectangular, fiber reinforced composite plate sujected to non-penetrating (low velocity) impact of a solid object. The plate may be simply supported or c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc94498a77956e06aca00b8fcfccd4d5
https://doi.org/10.1177/002199838802200603
https://doi.org/10.1177/002199838802200603