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二环[2.2.1]庚-5-烯-2-酮,1,7,7-三甲基-,(1S,4R)- | 15099-93-1

中文名称
二环[2.2.1]庚-5-烯-2-酮,1,7,7-三甲基-,(1S,4R)-
中文别名
——
英文名称
(1R)-bornen-(2)-one-(6)
英文别名
(1R)-Bornen-(2)-on-(6);Dehydrocampher;(1R,4R)-1,7,7-trimethylbicyclo[2.2.1]hept-5-en-2-one
二环[2.2.1]庚-5-烯-2-酮,1,7,7-三甲基-,(1S,4R)-化学式
CAS
15099-93-1;22516-10-5;104832-00-0
化学式
C10H14O
mdl
——
分子量
150.221
InChiKey
BQJYIYRCGDNPLN-XVKPBYJWSA-N
BEILSTEIN
——
EINECS
——
  • 物化性质
  • 计算性质
  • ADMET
  • 安全信息
  • SDS
  • 制备方法与用途
  • 上下游信息
  • 反应信息
  • 文献信息
  • 表征谱图
  • 同类化合物
  • 相关功能分类
  • 相关结构分类

物化性质

  • 沸点:
    197.0±9.0 °C(Predicted)
  • 密度:
    1.013±0.06 g/cm3(Predicted)

计算性质

  • 辛醇/水分配系数(LogP):
    1.9
  • 重原子数:
    11
  • 可旋转键数:
    0
  • 环数:
    2.0
  • sp3杂化的碳原子比例:
    0.7
  • 拓扑面积:
    17.1
  • 氢给体数:
    0
  • 氢受体数:
    1

SDS

SDS:d4602fd92101a6037eda8be07749eee9
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反应信息

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文献信息

  • Interlaminar fracture and low-velocity impact of carbon/epoxy composite materials
    作者:J. H. Hwang、O. Kwon、C. S. Lee、W. Hwang
    DOI:10.1007/bf02681828
    日期:2000.3
    The interlaminar fracture and the low-velocity impact behavior of carbon/epoxy composite materials have been studied using width-tapered double cantilever beam (WTDCB), end-notched flexure (ENF), and Boeing impact specimens. The objectives of this research are to determine the essential parameters governing interlaminar-fracture and damage of realistic laminated composites and to characterize a correlation between the critical strain energy release rates measured by interlaminar fracture and by low-velocity impact tests. The geometry and the lay-tip sequence of specimens are designed to probe various conditions such as the skewness parameter, beam volume, and test fixture. The effect of interfacial ply orientations and crack propagation directions on interlaminar fracture toughness and the effect of ply orientations and thickness on impact behavior ar-e examined. The critical strain energy release rare was calculated from the respective tests: in the interlaminar fracture test the compliance method and linear beam theory are used; the residual energy calculated from the impact test and the total delamination area estimated by ultrasonic inspection are used ill the low-velocity, impact test. Results show that the critical strain energy release rate is affected mainly by ply orientations. The critical strain energy release rate measured by the low-velocity impact test lies between the mode I and mode II critical strain energy release rates obtained by the interlaminar fracture test.
  • Asahina; Ishidate; Tsukamoto, Yakugaku Zasshi/Journal of the Pharmaceutical Society of Japan, 1936, vol. 56, p. 395,397
    作者:Asahina、Ishidate、Tsukamoto
    DOI:——
    日期:——
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