Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Takafumi Ishikawa"'
Autor:
Takafumi Ishikawa, Kenji Washio, Kensuke Kaneko, Xiao Rong Tang, Masaaki Morikawa, Tatsufumi Okino
Publikováno v:
Applied Phycology, Vol 3, Iss 1, Pp 120-131 (2022)
The red algal genus Laurencia produces abundant brominated metabolites, including cuparane- and laurane-type brominated sesquiterpenes. In order to gain insights into the biosynthesis mechanisms for brominated compounds, we focused on the vanadium-de
Externí odkaz:
https://doaj.org/article/75645c66f1e94829957d00f5249bae11
Autor:
Yuko Oguri, Mami Watanabe, Takafumi Ishikawa, Takashi Kamada, Charles S. Vairappan, Hiroshi Matsuura, Kensuke Kaneko, Takahiro Ishii, Minoru Suzuki, Erina Yoshimura, Yasuyuki Nogata, Tatsufumi Okino
Publikováno v:
Marine Drugs, Vol 15, Iss 9, p 267 (2017)
Six new compounds, omaezol, intricatriol, hachijojimallenes A and B, debromoaplysinal, and 11,12-dihydro-3-hydroxyretinol have been isolated from four collections of Laurencia sp. These structures were determined by MS and NMR analyses. Their antifou
Externí odkaz:
https://doaj.org/article/2ab925309a884a1893fced5a55147189
Publikováno v:
立教アメリカン・スタディーズ = Rikkyo American Studies. 43:115-138
Publikováno v:
Journal of the Japan Institute of Metals. 81:345-351
Publikováno v:
Journal of the Japan Institute of Metals. 80:691-696
Publikováno v:
Journal of the Japan Institute of Metals. 80:547-552
Autor:
Takafumi Ishikawa
Publikováno v:
The Annuals of Japanese Political Science Association. 70:1_96-1_116
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 52:289-294
As future space vehicles, Reusable Launch Vehicle (RLV) needs to be developed, where there are two kinds of RLV: Single Stage To Orbit (SSTO) and Two Stage To Orbit (TSTO). In the latter case, the shock/shock interaction and shock/boundary layer inte
Autor:
Hisaki Watari, Takafumi Ishikawa
Publikováno v:
The Proceedings of the Materials and processing conference. :707
Publikováno v:
Scopus-Elsevier
A new type of thermal protection device in hypersonic flight regime is proposed in this study. The device is installed on the booster (a delta wing) upper surface of a Two-Stage-ToOrbit (TSTO) model. The experimental study was first conducted here, a