نتایج جستجو برای: 0.012)

تعداد نتایج: 998  

2008
Eduardo D. Sontag

This paper discusses a theoretical method for the “reverse engineering” of networks based solely on steady-state (and quasi-steady-state) data.

2015
Alice B. Gottlieb James G. Krueger Mia Sandberg Lundblad Marie Göthberg Brett E. Skolnick Hiroyoshi Nishikawa

BACKGROUND The current trial was a first-in-human clinical trial evaluating the safety, tolerability, pharmacokinetics, pharmacodynamics, and preliminary efficacy of the recombinant monoclonal anti-interleukin-20 (IL-20) antibody, NNC0109-0012, which targets the inflammatory cytokine IL-20. METHODS In total, 48 patients aged 18 to 75 years with moderate to severe stable chronic plaque psorias...

2011
Ryotaro Inoue Kenta Muranaga Hideaki Takayanagi Eiichi Hanamura Masafumi Jo Tatsushi Akazaki Ikuo Suemune

Ryotaro Inoue, 2, ∗ Kenta Muranaga, Hideaki Takayanagi, 3 Eiichi Hanamura, Masafumi Jo, Tatsushi Akazaki, 2 and Ikuo Suemune 2 Dept. of Applied Physics, Tokyo Univ. of Science, Tokyo 162-8601, Japan. CREST, Japan Science and Technology Agency, Kawaguchi 332-0012, Japan. MANA, National Inst. for Materials Science, Tsukuba 305-0044, Japan. Japan Science and Technology Agency, Kawaguchi 332-0012, ...

2006
Yuma Kinoshita Ryo Namiki Takashi Yamamoto Nobuyuki Imoto

Yuma Kinoshita, 2, ∗ Ryo Namiki, 2 Takashi Yamamoto, 2 Masato Koashi, 2, 3 and Nobuyuki Imoto 2, 3 Division of Materials Physics, Department of Materials Engineering Science, Graduate school of Engineering Science, Osaka University, 1-3 Machikaneyama, Toyonaka, Osaka 560-8531, Japan CREST Reserch Team for Photonic Quantum Information, 4-1-8 Honmachi, Kawaguchi, Saitama 331-0012, Japan SORST Res...

Journal: : 2022

The efficiency of an airfoil can be improved by adjusting its surface. CFD software was used to investigate a 2D with and without spanwise semicircular groove on the upper NACA0012 airfoils grooves were analyzed using k-ω turbulence model. lift drag coefficients compared. To effect location efficiency, added in various locations compared smooth airfoil. flow velocity remained constant at 20 m/s...

2006
S. Sasaki S. Kang K. Kitagawa M. Yamaguchi S. Miyashita T. Maruyama H. Tamura T. Akazaki Y. Hirayama H. Takayanagi

S. Sasaki,1,* S. Kang,2,3 K. Kitagawa,4,3 M. Yamaguchi,1,3 S. Miyashita,5 T. Maruyama,5 H. Tamura,1,3 T. Akazaki,1,3 Y. Hirayama,1,6 and H. Takayanagi1,4,3 1NTT Basic Research Laboratories, NTT Corporation, Atsugi, Kanagawa 243-0198, Japan 2Institute of Physics, University of Tsukuba, Tsukuba, Ibaraki 305-8571, Japan 3CREST-JST, Honmachi, Kawaguchi, Saitama 331-0012, Japan 4Faculty of Science, ...

2006
Adam Miranowicz Şahin Kaya Özdemir Nobuyuki Imoto

Adam Miranowicz, 2, 3 Şahin Kaya Özdemir, 3, 4 Jǐŕı Bajer, Masato Koashi, 3, 4 and Nobuyuki Imoto 3, 4 Institute of Physics, Adam Mickiewicz University, 61-614 Poznań, Poland SORST Research Team for Interacting Carrier Electronics, 4-1-8 Honmachi, Kawaguchi, Saitama 331-0012, Japan Graduate School of Engineering Science, Osaka University, Toyonaka, Osaka 560-8531, Japan CREST Research Team for ...

2007
Takehito Yokoyama Shiro Kawabata Takeo Kato Yukio Tanaka

Takehito Yokoyama,1 Shiro Kawabata,2 Takeo Kato,3 and Yukio Tanaka1 1Department of Applied Physics, Nagoya University, Nagoya, Aichi 464-8603, Japan and CREST, Japan Science and Technology Corporation (JST), Kawaguchi, Saitama 332-0012, Japan 2Nanotechnology Research Institute (NRI), National Institute of Advanced Industrial Science and Technology (AIST), Tsukuba, Ibaraki 305-8568, Japan and CR...

نمودار تعداد نتایج جستجو در هر سال

با کلیک روی نمودار نتایج را به سال انتشار فیلتر کنید