Results 181 to 190 of about 9,950,957 (390)
Characteristic variation of Mach number in subsonic co-flowing jets by varying lip thickness. [PDF]
Kumar KS +5 more
europepmc +1 more source
ABSTRACT The article describes and reflects the development of a coherent interdisciplinary collection database management system of a large natural history museum. The internal and external requirements were analyzed and informed the technical development of the database. In parallel, staff skills increased and work routines were optimized.
Katrin Vohland
wiley +1 more source
Experimental and numerical investigation of suddenly expanded flow at sonic mach number. [PDF]
Khan A +4 more
europepmc +1 more source
Unsteady pressure and structural response measurements of an elastic supercritical wing [PDF]
Results are presented which define unsteady flow conditions associated with high dynamic response experienced on a high aspect ratio elastic supercritical wing at transonic test conditions while being tested in the NASA Langley Transonic Dynamics Tunnel.
Eckstrom, Clinton V. +2 more
core +1 more source
Study of a New Asymptotic Preserving Scheme for the Euler System in the Low Mach Number Limit
G. Dimarco, R. Loubère, M. Vignal
semanticscholar +1 more source
Abstract Did democratization reduce the likelihood of politically connected bank bailouts in the past? What role did private central banks play as independent lenders of last resort? To answer these questions, this article provides new detailed archival evidence on the causes of bank failures in Spain in July 1931.
Enrique Jorge‐Sotelo
wiley +1 more source
Mach number dependence of electron heating in high Mach number quasiperpendicular shocks
The efficiency of electron heating through microinstabilities generated in the transition region of a quasiperpendicular shock for a wide range of Mach numbers is investigated by utilizing particle-in-cell PIC simulation and model analyses. In the model analyses saturation levels of effective electron temperature as a result of microinstabilities are ...
openaire
Investigation of powered nacelles on a high aspect ratio NASA supercritical wing, phase 2 [PDF]
A modified wing with the long core separate flow nacelle and several E(3) nacelles was utilized. The effects of nacelle and pylon cant angles and nacelle longitudinal and vertical location were investigated over a Mach number range from 0.70 to 0.83. The
Flechner, S. G. +2 more
core +1 more source
The regulatory subunit RIβ of protein kinase A occurs in two variants that differ at residue 268 (A268 versus R268). This seemingly small substitution significantly changes cAMP sensitivity, basal kinase activity, and the dynamic behavior of the regulatory domains.
Maximilian Wallbott +6 more
wiley +1 more source

