Zobrazeno 1 - 10
of 24
pro vyhledávání: '"L. H. Back"'
Publikováno v:
Monographs on atherosclerosis. 15
Steady flow observations in a smooth curved femoral artery model with a gradual bend revealed a flow pattern like that observed in coiled pipes. A double helical type flow was found to develop, with converging streamlines in the wall vicinity from th
Publikováno v:
Journal of Clinical Investigation. 65:1498-1508
In vivo measurements of tissue oxygen tension were made at 10-micrometer intervals through functioning in situ rabbit femoral arterial walls, using inhalation anesthesia and recessed microcathodes with approximately 4-micrometer external diameters. E
Autor:
R. A. Seban, L. H. Back
Publikováno v:
Journal of Heat Transfer. 84:235-242
The effectiveness and the heat transfer have been measured in a system involving the tangential injection of air from a single spanwise slot into the turbulent boundary layer of an external air stream, with the velocity of the external stream increas
Autor:
L. H. Back
Publikováno v:
AIAA Journal. 8:794-802
Subsonic, transonic and supersonic laminar boundary layers acceleration and cooling effects, discussing heat transfer and gas enthalpy
Publikováno v:
Journal of Spacecraft and Rockets. 4:1040-1047
Turbulent boundary layer flow in conical supersonic nozzle, discussing convective heat transfer and adverse pressure gradient effect
Autor:
L. H. Back, E. J. Roschke
Publikováno v:
Journal of Applied Mechanics. 39:677-681
An experimental investigation of water flow through an abrupt circular-channel expansion is described over a Reynolds number range between 20 and 4200. The shear layer between the central jet and the reverse flow region along the wall downstream beha
Publikováno v:
AIAA Journal. 4:2226-2229
Convective heat transfer in accelerated heated air flows through cooled conical supersonic nozzles of three different configurations
Autor:
L. H. Back, R. A. Seban
Publikováno v:
Journal of Heat Transfer. 84:45-54
Velocity and temperature profiles are presented for the turbulent boundary layer downstream of a tangential injection slot for the further clarification of the film-cooling problem. The profiles refer primarily to an injection mass velocity of 0.36 t
Publikováno v:
AIAA Journal. 7:730-733
Turbulent boundary layer laminarization in conical nozzle flow, measuring velocity profiles and friction coefficient
Publikováno v:
Journal of Heat Transfer. 92:333-344
Boundary layer and heat transfer measurements are presented for flow through a cooled, conical nozzle with a convergent and divergent half-angle of 10 deg for a wall-to-total-gas temperature ratio of about 0.5. A reduction in heat transfer below valu