E
Ephraim Fischbach
Researcher at Purdue University
Publications - 286
Citations - 7039
Ephraim Fischbach is an academic researcher from Purdue University. The author has contributed to research in topics: Casimir effect & Neutrino. The author has an hindex of 36, co-authored 282 publications receiving 6693 citations. Previous affiliations of Ephraim Fischbach include Stony Brook University & University of Washington.
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Journal ArticleDOI
Possibility of measuring the thermal Casimir interaction between a plate and a cylinder attached to a micromachined oscillator
Ricardo S. Decca,Ephraim Fischbach,G. L. Klimchitskaya,Dennis E. Krause,Dennis E. Krause,Daniel Lopez,V. M. Mostepanenko +6 more
TL;DR: In this paper, the authors investigate the possibility of measuring the thermal Casimir force and its gradient in the configuration of a plate and a microfabricated cylinder attached to a micromachined oscillator.
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Estimating Parameterized Post-Newtonian Parameters from Spacecraft Radiometric Tracking Data
TL;DR: In this paper, the authors present a detailed covariance analysis of a spacecraft trajectory, analyzing uncertainties in the spacecraft state and parameters γ and β, including the effects of Earth and spacecraft relative geometries, station-location errors, stochastic accelerations, and uncertainties of the solar quadrupole moment J2.F or an X-band tracking system.
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Interaction of the K0-K0 system with external fields☆
TL;DR: In this article, the energy-dependence of the K 0 - K 0 parameters Δ m, τ S and η +− suggested by Fermilab regeneration data is analyzed phenomenologically.
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SU(3)-symmetric coupling of mesons to baryons and the strong D/F ratio
TL;DR: In this paper, pseudoscalar meson-baryon baryon (PBB) couplings are analyzed in both the Klein-Gordon (KG) and Duffin-Kemmer-Petiau (DKP) formalisms.
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Deflection of Spacecraft Trajectories as a New Test of General Relativity
TL;DR: In this article, the authors derived a simple formula which gives the general relativistic deflection of a spacecraft, idealized as a point mass, for all values of the asymptotic speed of the spacecraft.