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111.
112.
Flückiger 《Analytical and bioanalytical chemistry》1873,12(1):315-315
113.
114.
Flückiger 《Analytical and bioanalytical chemistry》1863,2(1):398-398
Analytical and Bioanalytical Chemistry - 相似文献
115.
G. Lunge A. Zeckendorf H. Wolpert H. Trautzsch J. Rosenthal O. Schulz W. Ohlmüller M. Müller J. B. Cohen G. Appleyard Fl Kratschmer E. Wiener Henriet W. Fossek M. Teich F. Clowes N. P. Schierbeck E. Cramer A. v. Bibra G. Defren Renk Hilger E. v. Raumer G. Gaglio Merget J. Uffelmann L. A. Nekam J. Archarow Kijanicin L. Eisenlohr Cl Fermi C. Arens H. Wegmann E. Knorr J. König und A. Bömer 《Fresenius' Journal of Analytical Chemistry》1897,36(1):329-340
Ohne Zusammenfassung 相似文献
116.
117.
A. Breakstone R. Campanini H. B. Crawley M. Cuffiani G. M. Dallavalle M. M. Deninno K. Doroba D. Drijard F. Eabbri A. Firestone H. G. Fischer H. Frehse W. Geist H. Flöge L. Gesswein G. Giacomelli R. Gokieli M. Gorbics M. Gorski P. Hanke M. Heiden W. Herr D. Isenhower E. E. Kluge J. W. Lamsa T. Lohse R. Mankel W. T. Meyer T. Nakada M. Panter A. Putzer K. Rauschnabel B. Rensch E. Rimondi M. Schmelling G. P. Siroli R. Sosnowski M. Szczekowski O. Ullaland D. Wegener R. Yeung 《Zeitschrift fur Physik C Particles and Fields》1987,33(4):475-481
Gluon scattering processes are studied in hadronic highp T events using data obtained with the Split Field Magnet detector (SFM) at the CERN ISR. The experimental set-up allowed the scanning of a wide range of parton energies and scattering angles. It is shown that for positive pions as trigger particles, the parton composition of the recoil jet is correlated with the polar angle and transverse momentum of the triggering pion. Over the kinematical region studied, the recoil jet originates predominantly from scatered gluons, with an increasing prevalence of the gluon component towards forward triggering angles. The variation of the momentum structure of the recoil jet with the trigger angle indicates that the fragmentation function of gluons is softer than that of quarks. 相似文献
118.
Based on the flux-tube-breaking mechanism, we have previously studied the strong decay of nonstrange baryons into the elastic and several inelastic channels. Here, we extend these studies toΔ π decay. We compare our results with those of Koniuk and Isgur and with recently improved experimental data. We also present results of a new and improved calculation ofN π decay and discuss the problem of resonance identification. 相似文献
119.
The title compound1 is found to be protonated corresponding topK
a
's of 2.5 and 0.5, thereby being two orders of magnitude less basic than bilatrienes-abc. Its deprotonation (pK
a
=17.1) is found to be less easy than in case of the bilatrienes.1 is shown to exhibit a very pronounced reactivity for nucleophiles at the methine positions 10 and 15—a thiole adduct and the 10,15-dihydroderivative of1 are isolated and characterised. In contrast to the bilatrienes the adduct formation is irreversible. Accordingly, no diastereomers at exocyclic double bonds could be produced photochemically. Complexation of the lactam oxygens is achieved in case ofLewis acids (eg. AlCl3), chelation after addition of a proton acceptor is observed in a few cases only (Zn++, Hg++, In+++).
Herrn Prof. Dr.K. Kratzl zum 70. Geburtstag gewidmet. 相似文献
120.
A class of feedback attitude-control systems which efficiently result in high-accuracy (10–4 radians), Earth-pointing motions of satellites of different configurations in elliptic orbits is developed. Gas jets provide the control torque. The state of the attitude motion is assumed to be completely known. Linear differential equations, which have time-varying coefficients and include terms for the gravity torque due to an oblate Earth and terms for the aerodynamic torque, are used to describe the attitude motion when the satellite is practically Earth-pointing. Pontryagin's maximum principle, the necessary conditions for exact solutions of optimal bounded-phase-coordinate problems, and guidelines obtained from the minimum-fuel attitude controls devised for single-axis systems are used in the development. The motions of somestable and someunstable satellites with the developed attitude-control systems are simulated on an analog computer. The overall control system, which is reliable as well as efficient, is simple to realize.This research was sponsored by the National Aeronautics and Space Administration under Grant No. G-133-61. 相似文献