Zobrazeno 1 - 10
of 12
pro vyhledávání: '"B. A. Lathrop"'
Publikováno v:
Frontiers in Earth Science, Vol 11 (2023)
Externí odkaz:
https://doaj.org/article/464fe46a403b4e2c92064f6cddf643b0
Publikováno v:
Frontiers in Earth Science, Vol 10 (2022)
The relationship between normal fault displacement (D) and length (L) varies due to numerous factors, including fault size, maturity, basin tectonic history, and host rock lithology. Understanding how fault D and L relate is useful, given related sca
Externí odkaz:
https://doaj.org/article/901c8af2f6d445fca51ef89c7c5d562a
Autor:
B K Lathrop, Rodney L. Biltonen
Publikováno v:
Journal of Biological Chemistry. 267:21425-21431
The Ca2+ requirement for lipid hydrolysis catalyzed by phospholipase A2 from Agkistrodon piscivorus piscivorus (App-D49) and porcine pancreas has been examined using small, unilamellar vesicles of dipalmitoylphosphatidylcholine (DPPC SUV). Hydrolysis
Publikováno v:
Methods in enzymology. 197
Future investigations into the role of the structure of phospholipid substrates and the interrelationships between substrate, calcium, and enzyme conformation in the activation process are clearly needed. Enzyme dimerization in the activation of phos
Publikováno v:
Advances in experimental medicine and biology. 279
Publikováno v:
Nuclear Science and Engineering. 88:71-76
Developpement de sections efficaces simples corrigees en temperature qui remplacent le systeme statique de Klein-Nishina. Deux parametres suffisent, avec une precision de deux decimales, pour reproduire explicitement les sections efficaces exactes da
Publikováno v:
Radiation Effects. 94:303-306
Publikováno v:
Current psychiatric therapies. 11
Autor:
B. L. Lathrop, R. E. Sennett
Publikováno v:
9th Structural Dynamics and Materials Conference.
Hypervelocity impact effect on structural honeycomb spacecraft wall configurations, stressing design and wall thickness parameters
Autor:
R. E. Sennett, B. L. Lathrop
Publikováno v:
Journal of Spacecraft and Rockets. 5:1496-1497
Hypervelocity impact effect on structural honeycomb spacecraft wall configurations, stressing design and wall thickness parameters