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First Report of Xenoroussoella triseptata Isolated from Soil in Korea
류정주,Seung-Yeol Lee,강인규,Leonid N. Ten,Hee-Young Jung 한국균학회 2022 韓國菌學會誌 Vol.50 No.3
A fungal strain, designated KNUF-20-NI009, was isolated from soil collected from Gunsansi, Jeollabuk-do, Korea. The isolate showed cultural features typical of the genus Xenoroussoella. Colonies cultivated on malt extract agar were olivaceous-brown to pale olivaceous-white at the margins, with undersides of dark olivaceous to olivaceous-brown and a white margin. The conidia, with a size range of 2.7-5.1×1.6-3.3 µm (x=3.6×2.6 µm, ̅ n=50), were globoid to ellipsoid in shape, hyaline when immature, becoming light brown to golden-brown when mature, and characterized by 1 or 2 guttules. Multi-locus sequence analysis based on a combined dataset of internal transcribed spacer regions (ITS), large subunit rDNA (LSU), small subunit rDNA (SSU), translation elongation factor 1-alpha (TEF1α), and RNA polymerase II largest subunit (RPB2) sequences revealed KNUF-20-NI009 to be a strain of Xenoroussoella triseptata. This is the first report of this species in Korea.
류정주,Ryu, Jeong-Ju 한국항공우주산업진흥협회 1997 航空宇宙 Vol.47 No.-
국내에서 생산된 항공기 및 관련 부품을 운용하기 위해서는 항공기 및 그것을 구성하고 있는 모든 부품의 제반 특성이 감항기준을 만족시킨다는 것이 입증되어 감함당국에 의해 승인되어야 한다. 항공기와 관련 부품의 승인은 법에 의한 감항 적합성 평가 절차를 따라야 하며, 이러한 평가 절차를 거쳐서 승인된 항공기는 비로소 감항성을 인정받아 운항이 허락되고, 또한 승인된 관련 부품은 항공기에 사용되어 최종적으로 고부가가치의 경쟁력을 얻을 수 있다.
정태은,박경하,류정주 대한기계학회 1995 대한기계학회논문집 Vol.19 No.9
The compressive tests under impact conditions were performed to establish a design guide for impact damage tolerance. The composition of layup was selected for the real cases of composite aircraft structure. The energy level of visible of visible damage threshold was determined as 7 Joules. It was found that the normalized bending stiffnesses in the direction of closely fixed boundary affected the area of damage. Graphite/epoxy used in the tests exhibited 60% reduction in compression strength at the energy level of visible damage threshold. Wet-conditioned specimens represented 9% reduction in residual compressive strength in comparison with room temperature ambient specimens. In this study, a design factor of 2.1 was proposed for the low velocity impact damage.